Glavkosmos

Launch provider Russia Verified
542 Products
1 Available Slots
41 Years Active
Visit website ↗

About Glavkosmos

Glavkosmos is the commercial subsidiary of Roscosmos State Space Corporation (the Russian Federal Space Agency), headquartered in Moscow, providing international commercial services including satellite launch, payload integration, procurement of Russian space equipment, cosmonaut training, and technical space cooperation for foreign customers. Established to manage foreign commercial sales of Russian space assets and services, Glavkosmos has coordinated launch agreements on Soyuz and other Russian launch vehicles, facilitated export of Russian space components and technologies, and supported international scientific cooperation with Roscosmos. The company serves foreign governments, commercial operators, and space agencies seeking access to Russian launch vehicles, space equipment, and professional cosmonaut training programmes.

Milestones

  • 1992 Russian Federal Space Agency established
  • 2015 Reorganized as the Roscosmos State Corporation
  • Operates Soyuz crew and Progress cargo missions

Capabilities

Carries 9
1U CubeSat3U CubeSat6U CubeSat12U CubeSatSmallSat <50 kgSmallSat 50–100 kgSmallSat 100–200 kgSmallSat 200–500 kg
Target satellites
up to 24 500 kg payload mass
Launch vehicles 5
Soyuz 2.1aSoyuz 2.1bAngara A5Soyuz 2.1b/Fregat-MSoyuz 2.1b/Fregat
Delivers to 7
LEOSSOPOMEOGTOHEOLO

Photos 2

Products

542

OrbiCraft 3D is an educational kit for nanosatellite platform design. The kit is delivered in a basic configuration with a flywheel for rotation in one axis. It can be updated by the 3-axis module. It is possible to complete the orientation and stabilization tasks with the help of the lifting bar us

1 6

«Terra» space flight simulation complex is delivered on conducting experiments with satellite models such as «OrbiCraft». Together with a kit, it allows to simulate a satellite flight in the Earth’s orbit. contains: RECOMMENDATION: 1 COMPLEX FOR 1 EDUCATIONAL SITE

1 10

Passive HF device of flight communication equipment.

1 6

Propellant - hydrazine. The unit consists of eight thermocatalytic low thrusters: 4 – main, and 4 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturing lead

1 3

Universal 3U CubeSat bus rated to 1500 km altitude, 3 kg dry mass, 2U/2.5 kg payload accommodation.

1 16

Passive HF device of flight communication equipment.

1 7

Glavkosmos product — A Set of Stationary Control and Verification Equipment (SSCVE). Details on request.

1 9

Version: strain gauge sensor. Type of protection - “Sealed enclosure”.

1 5

It is made according to "Regulation 98". Version: Strain gage sensor. Type of explosion protection - ”Sealed enclosure”.

1 5

It is made according to "Regulation 98". Version: inductive primary converter and amplifier, connected by an integral cable jumper L with a length of 0.15; 1.0; 1.5 m (depending on order). The type of explosion protection of the sensor is “Tight sheath”, cable jumper - “Intact cable network”.

1 5

Active suspension system for large-sized transformable spacecraft systems at ground modal testing. Simultaneously with the suspension, the dynamic parameters are estimated (velocity, acceleration, etc.) with reference to the absolute time scale.

1

Propulsive burn formation for center of mass velocity variation during spacecraft orbit control and braking.

1 11

Glavkosmos product — Aggressive Liquids Filling Equipment Complex. Details on request.

1 3

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The bearing is attached to the moving platform with small satellite or layout of satellite . Also the air bearing includes

1 3

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The bearing is attached to the moving platform with small satellite or layout of satellite. Also the air bearing includes a

1 3

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The bearing is attached to the moving platform with small satellite or layout of satellite. Also the air bearing includes a

1 3

Rotates through 360° along one axis (vertical), the possibility of rotation in two horizontal axises is limited. Air bearing consists of a pedestal and hemisphere-form bearing. The bearing is attached to the moving platform with small satellite or layout of satellite. Also the air bearing includes a

1 3

Use for spacecraft positioning in Space.

1 7

Analog transceiver circuit ORTD-LSN, together with DRT-LSN, is intended for use in the equipment of base stations and subscriber terminals of the local navigation system. Separately, VLSI ORTD-LSN can be used as the basis of the analog path in equipment for receiving and transmitting signals in the

1 9

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

1 3

All-ceramic active antenna module.

1 10

Glavkosmos product — Antenna ANT-406VA. Details on request.

1 10

Antenna components: - set of radiators; - instrumental part; - cable network.

1 2

Microstrip Active Antenna Module.

1 10

Microstrip Active Antenna Module.

1 10

Active geodesic antenna with rear radiation cut-off.

1 10

Active geodesic antenna with rear radiation cut-off.

1 10

All-ceramic active antenna module.

1 10

All-ceramic active antenna module.

1 10

Microstrip Active Antenna Module.

1 10

Microstrip Active Antenna Module.

1 10

Microstrip Active Antenna Module.

1 10

Microstrip Active Antenna Module.

1 10

The transceiver single-mirror antenna system includes an antenna with a 2.4 m reflector with an irradiating system, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting devices.

1 10

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 3.7 m reflector with an irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting devices.

1 10

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a reflector of 4.5 m with an irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting devices.

1 10

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 2.4 m reflector with a dual-band irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting dev

1 10

Microstrip Active Antenna Module.

1 10

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 6.0 m reflector with an irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting devices.

1 8

Glavkosmos product — Antenna Reflector Hold-down Lock (mechanical) Type 1. Details on request.

1 5

Component of the antenna hold-down system.

1 5

Dual Band Active Antenna Module.

1 10

The receiving two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a 4.1 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. Remote polarization switching. The structure does not include radio receivers

1 9

The two-mirror receiving and transmitting antenna system is constructed according to the Cassegrain system, it includes an antenna with a 7.2 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. The structure does not include radio receive

1 10

The receiving two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a 7.2 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. Remote polarization switching. The structure does not include radio receivers

1 9

The receiving two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a 7.2 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. Remote polarization switching. The structure does not include radio receivers

1 8

The receiving two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a 7.2 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. Remote polarization switching. The structure does not include radio receivers

1 9

The receiving two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a 9.3 m reflector with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. Remote polarization switching. The structure does not include radio receivers

1 8

Dual band active antenna module.

1 10

AFD 137 MHz, AFD 150 MHz and AFD 400 MHz.

1 3

Glavkosmos product — Antenna-feeder Device (AFD) MBITS-01. Details on request.

1 3

Transmitting antennas, receiving antennas, feeder, matching devices, power control filters.

1 3

Transmitting antenna, feeder, matching control device.

1 3

Glavkosmos product — Antenna-feeder Device BASN. Details on request.

1 3

Glavkosmos product — Antenna-feeder Device BIS-MV. Details on request.

1 3

Component of large antenna systems.

1 9

2 receiving antennas, 2 transmitting antennas, feeder network.

1 3

The transceiver two-mirror antenna system is constructed according to the Cassegrain system, it includes an antenna with a 9.3 m reflector with an irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transm

1 10

AFS are used to transmit signals in radio communication systems, broadcasting, television, as well as other radio systems using radio waves to transmit signals. The function of an antenna is to emit or receive electromagnetic waves. The electrical connection of the antenna to the source (consumer) c

1

Lens objectives for astronomic telescopes with special-dispersion glass, adaptable clear aperture and focal distance.

1 10

Monoblock equipment for regulation and monitorung of the manned spacecraft’s power supply system. It is possible to change the design of the monoblock to increase power up to 10 kW by layout of internal submodules. It is planned to operate as part of a perspective piloted transport system.

1 9

Two-phase (vapor/liquid) hermetic closed evaporating/ condensing thermal transfer system filled with a working fluid (Toluene, Ammonia, Propylene, Ethane, Methane, Nitrogen) of straight or complicated configuration.

1 5

Light-weighted aspherical mirrors made of low-CTE Sitall glass-ceramic for ground-based and space optical systems.

1 10

Asperical mirror Specific features: Item is produced in accordance with the Customer's working design documentation (WDD).

1 1

The asynchronous controlled electric motor has a 2-phase supply voltage of 40 V, 1000 Hz; the speed of rotation is not less than 16000 rpm; the minimum operating time is 150 hours.

1 3

Pneumatic automation equipment.

1 4

Propellant - hydrazine. The unit consists of two modified thermocatalytic low thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturin

1 3

Propellant - hydrazine. The unit consists of two thermocatalytic low thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturing lead ti

1 3

Glavkosmos product — Automated System for Launch Complex Ground Support Equipment Control. Details on request.

1 7

Glavkosmos product — Automated Testing Complex ATC. Details on request.

1 14

Automatic control system of thermal-vacuum-testing for spacecraft.

1 5

Glavkosmos product — Autonomous Measurements System. Details on request.

1 2

Glavkosmos product — Axial Grooved Heat Pipes. Details on request.

1 5

Passed a full cycle of testing according to the European standard PSS49 and flight applications from European, Chinese and American partners. The arterial design of the capillary structure allows you to increase the power of heat pipes without increasing their mass characteristics, to increase their

1

Sealed monoblock device including 3 small fiber optic gyroscopes and a set of electronic devices.

1

Glavkosmos product — BELKA-2 Research Equipment. Details on request.

1

Glavkosmos product — Bipropellant Low Thrust Rocket Engine. Details on request.

1

Propellant storage and feed to liquid propellant thrusters.

1 9

Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands.

1 10

Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands. Design features: - A high temperature Niobium alloy nozzle with disilicide oxidation resistant coating.

1 10

Glavkosmos product — Bipropellant Thruster 17d. Details on request.

1 10

HF element of the antenna feed system paths.

1 8

Glavkosmos product — C-band Antenna which Forms Planimetric Directional Diagram. Details on request.

1 6

HF element of the antenna feed system paths.

1 2

Glavkosmos product — C-band Global-beam Antenna. Details on request.

1 5

Glavkosmos product — Capacitor K50-80. Details on request.

1 5

Glavkosmos product — Capacitor K50-81. Details on request.

1 5

Glavkosmos product — Capacitor K50-83. Details on request.

1 5

Glavkosmos product — Capacitor K50-84. Details on request.

1 5

Glavkosmos product — Capacitor K50-85. Details on request.

1 5

Glavkosmos product — Capacitor K50-87. Details on request.

1 5

Glavkosmos product — Capacitor K50-88. Details on request.

1 5

Glavkosmos product — Capacitor K50-89. Details on request.

1 5

Aluminum electrolytic capacitors.

1 5

Glavkosmos product — Capacitor K50-91. Details on request.

1 5

Glavkosmos product — Capacitor K50-92. Details on request.

1 5

Glavkosmos product — Capacitor K52-11. Details on request.

1 5

Glavkosmos product — Capacitor K52-17. Details on request.

1 5

Glavkosmos product — Capacitor K52-18. Details on request.

1 5

Glavkosmos product — Capacitor K52-19. Details on request.

1 5

Glavkosmos product — Capacitor K52-20. Details on request.

1 5

Glavkosmos product — Capacitor K52-21. Details on request.

1 5

Glavkosmos product — Capacitor K52-9. Details on request.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Tantalum solid-electrolyte capacitors.

1 5

Glavkosmos product — Capacitors K50-96. Details on request.

1 5

Glavkosmos product — Capacitors K50-97. Details on request.

1 5

Glavkosmos product — Capacitors K50-98. Details on request.

1 5

Glavkosmos product — Capacitors K58-26. Details on request.

1 7

A cart, can be pulled either manually or by a vehicle.

1 4

Technology for manufacturing mirror antennas of caisson type with reduced reflector surface density.

1 6

Charged particle detector was developed by Sputnix in collaboration with scientists from SINP (Moscow State Univercity). Detector provides simultaneous monitoring and single events parameters measurement. Recorded data can be accessed via satellite data bus.

1 10

Glavkosmos product — Cold Ammonia Corrective Propulsion System. Details on request.

1 5

Glavkosmos product — Complex IVK-M. Details on request.

1 17

Glavkosmos product — Complex IVK-SOK-M. Details on request.

1 13

Glavkosmos product — Complex of Technical Means for Impact Area Operation. Details on request.

1 5

Propellant storage and feed to electrical thruster

1 9

Storage and feed of pressurant to propellant tanks and operating fluid to cold gas thrusters

1 10

Compressed Gases Storage Equipment (CGSE) includes 210 bottles, incorporated in 6 receiver blocks; nitrogen charging boards; air charging boards; nitrogen supply boards; air supply boards; helium charge and supply board; quality control board; hygrometer; oil indicator; gas pressure monitoring board

1

LV Compressed gases supply system (LV CGSS, CGSS) includes distribution boards; purging boards, auxiliary boards; supply boards; control boards; control pressure boards; panels; pressure sensor units; pressure gage panels; parameters monitoring boards; pressure reduction boards; quality control boar

1

Flight-proven CFRP conical adapter (650 mm) interfacing spacecraft to the Briz-M upper stage on Proton.

1 8

Flight-proven CFRP conical adapter (398.5 mm, 34 kg) interfacing spacecraft to the Fregat-SB upper stage on Zenit.

1 8

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

1 7

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

1 7

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

1 7

Two-phase (vapor/liquid) hermetic closed evaporating/ condensing thermal transfer system filled with a working fluid (usually by Ammonia or Propylene). Small pipes diameter allows to bend transport lines that simplifies essentialy CHP integration into the spacecraft; Condensers of different design (

1 5

Programmable control complex of large-sized product forms in real time. The principle of operation is based on measurement of the product shape deviation from the a predetermined value using a network of compact triangulation distanse sensors, mounted on the stocks near the control points of the obj

1 7

The software package operation is limited to control of colour array of spacecraft structural function diagram, obtained as a result of proccessed telemetric data. In case of onboard system alarm state, an operator can analyze current situation using output ducuments or a graph of selected parameter

1

Software package featuring the following functions: -Virtual machine creation and control; - Distributed fail-safe storafe of virtual machines; - High availability of virtual machines and package elements; - Package automatic installation and setting; - Common control web-interface; - Terminal devic

1

Glavkosmos product — Cool Gas Thruster. Details on request.

1 10

Consists of two units: Stationary Plasma Thruster with a nominal discharge power of 1350 W and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6

1 10

The corrective propulsion system of the UD-AIPD consists of a monoblock, including the KNE block, the BIR1, BIR2 block, and the discharge accelerator channel. UD-AIPD includes a set of mounting parts. The operating mode of the UD-AIPD is pulse with a pulse repetition rate of 4 Hz.

1 7

Corrective propulsion system (CPS) consists of a monoblock, including an AIPD-95 CPS engine, a BPU-150 device, a set of mounting parts. The CPS AIPD-95 engine includes a KNE block, a BIR1, BIR2 block. CPS AIPD-95 is equipped with KIA CPS. The operating mode of the AIPD-95 CPS is pulsed with a pulse

1 7

Crossbeam with the device for loading beam and load system aligning.

1 3

Crossbeam with the device for kinematic compensation of loads interacting when mating.

1 2

Glavkosmos product — CubeSat ADCS Testing Facility. Details on request.

1 9

Ground complex provides two-way communication with small spacecraft.

1 6

Glavkosmos product — DC/DC Converter. Details on request.

1 4

Component of large antenna systems.

1 5

Component of large antenna systems.

1 7

It is made according to "Regulation 88". Version: piezoelectric transducer, consisting of a sensitive element installed in the housing, and a matching device connected by a cable jumper. Explosion protection type - "Intrinsically safe electrical circuit" - is provided by an intermediate converter.

1 5

It is made according to the "Regulation 98". Version: piezoelectric transducer, consisting of a sensor installed in the housing, a flexible cable and a connector. Explosion protection type - "Intrinsically safe electrical circuit" - is provided by an intermediate converter.

1 5

Glavkosmos product — Digital Isolator. Details on request.

1 4

High performance digital signal processor. The processor architecture is based on the use of the new generation VLIW / SIMD processor core NMC4. The processor contains two processor cores NMPU0 and NMPU1, each of which includes a RISC processor and a vector coprocessor.

1 7

Glavkosmos product — Double-mirror Ka-band Parabolic Antenna. Details on request.

1 6

Dual operating mode: 1.35 / 2.5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 100 mm. Mean diameter of the accelerating channel is 85 mm.

1 10

Version: strain gauge sensor with cable jumper. Upon customer's request, it is made with a screwed fitting and a collar (Ø32) for welding or only with a screwed fitting. The type of explosion protection of the sensor is “Tight sheath”, cable jumper - “Intact cable network”.

1 5

The System consists of pneumoboards; pressure indicator unit; pressure sensor unit; drainage pneumoboard; three manifolds; set of pipelines and valves.

1

Single-stage, multi-starting, normally closed, single-seat, teflon seal solenoid valve.

1 9

EH is a flexible single-sided printed circuit board on a thin, dielectric base made of fiberglass or polyimide film with a resistive printed conductor made of manganin foil of a certain configuration deposited on it. A protective dielectric coating of a polyimide film or varnish is applied over the

1 5

The electric heater is a flexible single-sided printed circuit board on a thin, dielectric base made of fiberglass with a resistive printed conductor made of manganin foil of a certain configuration deposited on it. A protective electrical insulating coating is applied over the conductor.

1 5

Electric propulsion. It has high specific impulse at relatively low power. The record number of burnings is up to 20000 cycles.

1 5

Electric propulsion. Record specific impulse and propulsion resource for Hall-effect thrusters.

1 5

Electric propulsion. High specific impulse. Cathodes on the basis of W-Ba emitter.

1 5

Electric propulsion. Multimode thruster. Cathodes on the basis of W-Ba emitter.

1 5

Electric propulsion. It has high efficiency at low power.

1 5

Sustainer power thruster for spacecraft.

1 5

Electrolysis unit for oxygen supply system.

1 4

The core electromagnet for the stabilization equipment of the spacecraft with a harness on which the connector is soldered.

1 4

Electromagnetic unit (EMU) - Magnetic Torquer There is an option to develop and supply EMU with magnetic moment from 0.2 to 800 А·m² according to customer requirements

1 9

Electromagnetic unit (EMU) - Magnetic Torquer for nanosatellites. There is an option to develop and supply EMU with magnetic moment from 0.2 to 2 А·m² according to customer requirements.

1 9

Includes: GLONASS/GPS receiver with antenna, 406.037 MHz and 121.5 MHz transmitters, the voice communication device (121.5 MHz radio station), AНT-AРM-2 antenna, the liquid crystal indicator for displaying position data and service information, highlight, self-contained power source (battery, accumu

1 5

Glavkosmos product — Equipment for determing the center-of-mass position and inertia characteristics of nanosatellites. Details on request.

1 2

In accordance with the specification of the customer.

1 5

Component of the Ku-band multiple-beam antenna.

1 4

Component of the C-band antenna which forms planimetric directional diagram.

1 3

Component of the large Ku-band antenna system with planimetric directional diagram.

1 3

Elements of antenna feed system and flight communication equipment paths of different frequency bands.

1 6

Version: strain gage sensor, consisting of a cylindrical type elastic element, strain gages connected in two bridge circuits, a casing, a power input unit and a plug. Type of protection - “Intrinsically safe electrical circuit” - is provided by an intermediate converter.

1 5

Uses GaAs photo-electric converters and has built-in electromagnetic coils. Features: There is a 13 mm diameter aperture at the panel center with M2 mount holes for sun sensors or similar payloads.

1 10

Uses GaAs photo-electric converters and has built-in electromagnetic coils.

1 10

Pneumatic automation equipment.

1 6

Glavkosmos product — Glazing of Spacecraft. Details on request.

1 3

The navigation receiver is designed to calculate the current coordinates and speed of an object in real time in stand-alone and differential modes, form a second time stamp and exchange information with external equipment using RS232 interfaces. It is an electronic module of zero level in accordance

1 29

Glavkosmos product — GNSS Receiver in a Secure Enclosure. Details on request.

1 29

The receiving dual-band mirror antenna system is built on the Cassegrain system, includes an antenna with a reflector of 2.5 m, two replaceable irradiating systems of the C and Ku bands, and a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transm

1 9

The transmitting two-mirror antenna system is built on the Cassegrain system, it includes an antenna with a reflector of 2.5 m with an irradiating system and a counter-reflector, and a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting d

1 7

The receiving two-mirror antenna system is constructed according to the Cassegrain system, it includes an antenna with a 12.0 m reflector with replaceable irradiators and a counter-reflector, a slewing ring with electromechanical drives. Remote polarization switching. Replaceable irradiators: C-band

1 8

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 2.4 m reflector with an irradiating system and a counter-reflector, and a slewing gear with manual drives. The structure does not include radio receivers and radio transmitting devices.

1 9

The transceiver two-mirror antenna system is built on the Cassegrain system, includes an antenna with a 6.0 m reflector with an irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transmitting devices.

1 10

The transceiver two-mirror antenna system is constructed according to the Cassegrain system, it includes an antenna with a 6.0 m reflector with a dual-band irradiating system and a counter-reflector, a slewing ring with electromechanical drives. The structure does not include radio receivers and rad

1 10

The receiving dual-band mirror antenna system is built on the Cassegrain system, includes an antenna with a reflector of 2.5 m, two replaceable irradiating systems of the C and Ku bands, and a slewing ring with electromechanical drives. The structure does not include radio receivers and radio transm

1 9

Ground control station for working with spacecraft.

1 8

Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. Sealed monoblock device, including electronic and optoelectronic modules with a block of four sensitive elements of a fiber-optic gyroscope and four sensitive elements of pendulu

1 9

Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. Sealed monoblock device, including electronic and optoelectronic modules with a block of four sensitive elements of a fiber-optic gyroscope and four sensitive elements of pendulu

1 9

Monoblock device includes electronic and optoelectronic modules and a block of sensitive elements containing three mutually orthogonal sensitive elements of a fiber-optic gyroscope.

1 5

Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. An unsealed two-block construction including an electronic device unit with four independent channels consisting of electronic and optoelectronic modules and an inertial unit con

1 4

High precision drive with the gear wheel.

1 5

High precision drive with the gear wheel.

1 5

Glavkosmos product — Helical-beam Antenna. Details on request.

1 6

Glavkosmos product — High Precison GNSS module. Details on request.

1 10

Pneumatic automation equipment.

1 6

High voltage power supply system kit KPVS includes: The ability to configure the power supply system for power from 2 to 60 kW by increasing or decreasing the number of modules. It is planned to operate as part of the scientific and energy module of the International Space Station (ISS).

1 4

Glavkosmos product — High-capacity Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure. Details on request.

1 9

Electric propulsion. Multimode thruster. Cathodes on the basis of W-Ba emitter.

1 5

Glavkosmos product — High-precision automated angle-setting complex. Details on request.

1 8

The High-speed X-band Downlink Transmitter with throughput up to 880 Mbps.

1 8

System of pipelines, valves and other equipment located in launch facility.

1

Honeycomb panels with composite face sheets, with fixed or attachable heat transfer tubes or fluid loops. Off-the-shelf efficient solutions include standard series of honeycomb fillers and face sheets, filling blocks; possibility of installing heat transfer tubes or fluid loop tubes; mounting of opt

1 6

Glavkosmos product — Horn Antenna. Details on request.

1 4

Mobile Hydrogen Peroxide Tanker includes vessels for high-concentrated hydrogen peroxide (HCHP), vessel for demineralized water, vessel for industrial water, electric equipment, pneumatic and hydraulic equipment, HCHP temperature and volume control means, compressed air bottles, stop valves.

1 3

Sealed monoblock device including electronic and opto-electronic modules with a block of sensitive elements, containing three mutually orthogonal sensitive elements of fiber-optic gyroscopes and three of mutually orthogonal sensitive vibrating string accelerometer elements.

1 2

Glavkosmos product — Integrated Circuit 1879 ВМ8Y. Details on request.

1 7

Glavkosmos product — Integrated Circuit 1888 TX 018. Details on request.

1 7

ITU-5000M includes a high-precision Thruster Orientation Mechanism (TOM) and a propulsion system based on the Modified Stationary Plasma Thruster with a discharge power of up to 5 kW. Each propulsion system consists of a thruster and a XFC Unit, pneumatic connections between which are realized by me

1 8

Integrated Thruster Unit (ITU) includes a high-precision thruster orientation mechanism (TOM) and two propulsion systems based on the stationary plasma thruster with a nominal discharge power of 1350 W. Each propulsion system consists of a thruster and a Xenon Flow Controller Unit, pneumatic connect

1 8

A stand with mechanical drive, which allows to to set the angle of inclination of the Product in any position with high accuracy.

1 4

Glavkosmos product — Integration Stand 2. Details on request.

1 4

Glavkosmos product — Interface Module with Application Processor. Details on request.

1 10

Optical communications equipment for work in the constellation of satellites at the same height. Monoblock design. Adaptation to any platform with a weight of 300 kg.

1 9

Optical communications equipment between satellites on LEO and between LEO and Earth. Adaptation to any platform with a weight of 400 kg.

1 9

Glavkosmos product — IVK-01N Complex. Details on request.

1 12

Glavkosmos product — Ka-band Antenna for the Locator Beacon Signal Transmission. Details on request.

1 5

Glavkosmos product — Ka-band High-precision Antenna. Details on request.

1 5

System consists of tanks, pumping equipment, pipelines, valves and control means.

1 3

Set of pipelines, valves and different kind of equipment located inside launch facility and on MST.

1

The System consists of pipelines, valves and other equipment and located inside Launch Facility.

1

Glavkosmos product — Kinetic Moment Reset System. Details on request.

1 4

Kinetic moment reset system. Structurally, the product consists of: - 2 primary converters of the geomagnetic field PGP-3M, PGP-3MD (duplicate); - 3 electromagnets (length - 0.85 m), forming three axis rod electromagnets; - electronic block.

1 4

Glavkosmos product — Ku-band Multiple-beam Antenna. Details on request.

1 1

Attenuator (ATT) is designed to control the amplitude of the input signals of the L-band. The MMIC is developed on the basis of silicon-germanium BiKMOS technology. MMIC ATT is a parallel-serial chain of resistive blocks, switched using MOS keys. An amplifier has been added to the circuit to obtain

1 12

MMIC phase shifter (PS) controls the phase of the input signals of the L-band. MIS is developed on the basis of silicon-germanium BiKMOS technology. The basis of the MIS FV circuit design is the vector addition of orthogonal signals. MMIC has differential inputs and outputs. Phase states are control

1 14

SiGe (Silicon-germanium) BiKMOS microwave MMIC mixer implements the Gilbert active mixer circuit. The microcircuits are designed to operate as a mixer of the receiving and transmitting paths in the frequency range up to 2 GHz, with a possible extension of the band to 4 GHz.

1 14

MMIC LNA is designed for equipment with severe restrictions on the level of power consumption, including: Due to the capabilities of BiKMOS circuitry and the high speed of silicon-germanium transistors, silicon-germanium BiKMOS microwave MMIC LNA has significantly lower power consumption compared to

1 12

polarization selection of received signals and forming required polarization of the radiated signals

1 4

Long-focus lens objective (500 mm aperture, 4000 mm focal distance) for Earth remote sensing equipment.

1 8

LS is a metal structure on which the equipment as follows is assembled: 4 Frames for ILV weight load taking; 4 Frames for ILV holdup when wind forcing; 2 Masts for supply lines connexion to ILV. Inside the frame basements the sets of electric and hydraulic equipment for the Frames motion provision a

1

Short-focus lens objectives (40 mm aperture, 40-200 mm focal distance) for Earth remote sensing payloads.

1 8

Wide-angle 13-lens objective for detection of low-orbit space objects at altitudes from 120 to 500 km.

1 12

High precision electromechanical drive of linear positioning. 2 commutator electric motors (1 is in reserve).

1 8

System includes tanks, pipelines, valves and control means located in different facilities of Launch Complex.

1 3

System includes equipment as follows: tanks, pipelines, valves and control means.

1 3

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 10

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 10

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 11

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 11

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 11

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 11

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

1 10

Pneumatic automation equipment.

1 6

HF element of the antenna feed system paths.

1 2

Plasma thruster. Propellant - xenon. Consists of the anode and cathode units. With hollow cathode. Development status – engineering model. Mean diameter of the accelerating channel is 34 mm. New structural materials and components. Manufacturing lead time is given without taking into account the tim

1 10

Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and three external magnetic coils. Outside diameter of the accelerating channel is 50 mm. Mean diameter of the accelerating channel is 40 mm. Manufacturing lead time i

1 10

Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is 55 mm. Manufacturing lead time is

1 10

Pneumatic automation equipment.

1 6

Heat pipe with axial omega-shaped grooves. Heat carrier ammonia.

1 3

Devices are used as switchboards, power distribution points, control and automation panels and cabinets, and as switchboards on the undervoltage side of packaged transformer stations.

1

Glavkosmos product — LV Thermal Conditioning System [high pressure]. Details on request.

1

Glavkosmos product — LV Thermal Conditioning System [low pressure]. Details on request.

1

System of three pairs of square coils mutually orthogonal to each other (Helmholtz cage) simulates the magnetic field as it changes during the orbital flight the satellite. By inducing current in coil’s wires the magnetic field is created and its direction and value depend on the amperage. Currents

1 3

Device for manual start-up of pico and nanosatellites from International Space Station (ISS). Supplied with remote control. There is an option to develop and supply a launch device for automatic launch in any orbit.

1 8

Leak is determined by the helium flow penetrating into the tested volume during the vacuum test, or by the flow of helium going from the tested volume at a excessive pressure in it.

1 10

Glavkosmos product — MDM microwave varactors. Details on request.

1 7

T-406Н КС tester represents a compact portable device. T-406Н КС tester is able to receive radio signals both over the air, when antenna is attached, and over coaxial cable. Self-contained power is supplied by built-in rechargeable battery with the total voltage equal to (3.7 V ± 10%) and capacity n

1 5

Component of the hold-down system.

1 6

Two-degree-of-freedom electromechanical drive for antenna pointing.

1 10

Two-degree-of-freedom electromechanical drive for antenna pointing.

1 10

Two-degree-of-freedom electromechanical drive for antenna pointing.

1 10

Two-degree-of-freedom electromechanical drive for antenna pointing. Operating regimes: tracking, pointing.

1 10

Glavkosmos product — Metal Composite Xenon Tank XT-200. Details on request.

1 7

Glavkosmos product — Metal Composite Xenon Tank XT-350. Details on request.

1 7

Glavkosmos product — Micropower ADC. Details on request.

1 7

Silicon-Germanium BiKMOS VLSI is designed to produce a stable high-frequency signal in the 375-6000 MHz range with a low level of phase noise and a small tuning step without using an external VCO. Functional Analog: ADF4350 (Analog Devices Inc.)

1 13

Glavkosmos product — Microwave p-i-n elements. Details on request.

1 7

Glavkosmos product — Mirror Antenna. Details on request.

1 4

Component of the mirror antenna. If required mounting reflector on the boom is available Reflectors have areas for hold-down locks and are equipped with optical checking elements.

1 6

Large-dimensioned mirror-lens objectives. Item is produced in accordance with the Customer's working design documentation (WDD).

1 2

Passive HF device of flight communication equipment.

1 4

Passive HF device of flight communication equipment.

1 4

Passive HF device of flight communication equipment.

1 4

The station includes an antenna system with a 2.4 m Ku-band reflector. The design is collapsible, transported in containers from the station. It provides point-to-point communication through the Luch spacecraft.

1 10

MST is a mobile weather-proof and self-propelled structure, which can travel inside the launch facility on two parallel railway tracks consisting of two rails each due to traveling gear representing four self-propelled balance trucks. MST is equipped with the gates at its front and rear ends, statio

1 2

Passive glass retroreflector spherical satellite used to calibrate quantum-optical ground stations.

1 3

Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and three external magnetic coils. Outside diameter of the accelerating channel is 50 mm. Mean diameter of the accelerating channel is 40.5 mm. Low flow rate cathode.

1 10

In terms of discharge power it has been forced up to 1250 W. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system of armored type with magnetic screens. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is

1 10

Thruster with a discharge power of up to 5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and eight external magnetic coils. Outside diameter of the accelerating channel is 140 mm. Mean diameter of the accelerating chann

1 10

Thruster with a nominal discharge power of 1350 W. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 100 mm. Mean diameter of the accelerating ch

1 10

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a nozzle, a propellant injection unit, two small-size solenoid valves that supply propellant to the thruster, and a pressure signaling indicator that monitors the fact that the thruster

1 10

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a nozzle, a propellant injection unit, two small-size solenoid valves that supply propellant to the thruster, and a pressure signaling indicator that monitors the fact that the thruster

1 8

Propellant storage and feed to liquid propellant thrusters.

1 9

Represents a Raspberry-Pi Compute Module carrier which contains a set of devices.

1 9

Represents a Raspberry-Pi Compute Module carrier which contains a set of devices.

1 9

Represents a Raspberry-Pi Compute Module carrier which contains a set of devices.

1 9

Bellows are manufactured of corrosion-resistant and fire-resistant steel grades 08Х18Н10Т or 12Х18Н10Т. They provide complete leak-tightness at high pressures and temperatures in combination with excellent flexibility, which is particularly important for hazardous industries.

1 5

Strength and thermal honeycomb panels with Aluminum and carbon fibre skins and honeycombs made of Aluminum foil. Thermal honeycomb panels contain embedded and manifold heat pipes, liquid loops, thermal optical coatings of different types, heaters, thermal sensors, multi-layer insulation.

1 3

Multi-layer honeycomb panels with fixed or attachable heat transfer tubes or fluid loops. off-the-shelf efficient solutions include standard series of honeycomb fillers and face sheets, filling blocks; possibility of installing heat transfer tubes or fluid loop tubes; mounting of optical solar refle

1 4

Glavkosmos product — Multi-zone Electrical Furnace «MEF-01». Details on request.

1

Electrically powered multichannel thruster for spacecraft.

1 5

Glavkosmos product — Multicontroller 1888 BC 048. Details on request.

1 11

Component of the mirror antenna. A feed of this type as a component of the offset mirror antenna provides formation of the narrow beams set for the specified servicing area in order to enhance signal for the specified subscribers.

1 5

Glavkosmos product — Nanosatellite Attitude Control. Details on request.

1 6

Glavkosmos product — Nanosatellite Battery Array. Details on request.

1 5

For debugging used UART interfaces with galvanic isolation between PC and nanosatellite .

1 5

Glavkosmos product — Nanosatellite Electrical Power System. Details on request.

1 6

Ground-based nanosatellite engineering model for developing and testing scientific payloads, software and onboard systems.

1 8

Glavkosmos product — Nanosatellite Onboard Computer. Details on request.

1 8

Radiation-resistant components.

1 8

SamSat 3U CubeSat platform for scientific and technological experiments, with ~2 dm³ of payload volume.

1 13

Glavkosmos product — Nanosatellite Solar Panel. Details on request.

1 6

Glavkosmos product — Nanosatellite Transceiver. Details on request.

1 5

Glavkosmos product — Navigation and Communication Module. Details on request.

1 8

The Systems includes pneumovalve unit; purge and pressure control board; control pneumoboard; pressure indicator and sensor board.

1

Equipment Set consists of: - set of power connectors; - set of cables and low-voltage packaged devices.

1 2

Efficient manufacturing technology of antennas with a complex mechanical interface.

1 4

Structurally available in 4 versions:

1 29

Component of large antenna systems.

1 5

The On-board Memory Unit is designed to provide data storage for the remote sensing satellites payloads.

1 7

Infrared instrumentation for measuring the spectra of outgoing thermal radiation of the surface-atmosphere system with high spectral resolution in the interests of operational meteorology and climatology.

1 10

Glass plate. Optical glass doped with cerium K-208 OST3-3677-82.

1 1

Ground contact point with spacecraft at LEO. Mobile design, placement on roofs of buildings and other non-specialized objects is possible. Mobile and stationary performance, adaptation for any support.

1 9

Glavkosmos product — Optoelectronic system of detection and measurement of space debris motion. Details on request.

1 6

Glavkosmos product — P-band Global-beam Antenna. Details on request.

1 6

The vacant area of the board is 2.54mm pitch breadboard where user can place any needed components to enable payload’s sensors and other periphery. Holds a MCU with CAN driver, which grants access to the satellite bus. The possibility to modify hardware and software by the customer.

1 9

Glavkosmos product — PCI Express Chip 1888 BB 018 A. Details on request.

1 6

Comprises: GLONASS/GPS receiver with an antenna, ПРД-406 transmitter, ПРД-121 transceiver, AНT-AРM-02 transmitting-receiving antenna, the indicator for position and service data displaying, self-contained power supply, rechargeable battery, and charger. The radio beacon can be completed with hermeti

1 5

Glavkosmos product — Photomultiplier Tube. Details on request.

1 8

Glavkosmos product — Photomultiplier Tube 1. Details on request.

1 9

PMT-188 has bialkali photocathode and one-cascade multiplication system. The input window is made of boron-silicate UV glass.

1 10

PMT-tetrode has a bialkali photocathode and two-cascade multiplication system. The input window is made of boron-silicate UV glass

1 10

Version: piezoelectric sensor, consisting of a sensor installed in the housing, and a flexible cable.

1 5

Version: forced-cooling piezoelectric sensor, consisting of a sensor installed in the housing and a flexible cable.

1 5

Platform for cubesat 3U satellite installation contains all necessary items for entire microsatellite integration to provide its tests via test bench. Platform consists of structure and balancing system.

1 2

Glavkosmos product — Platform for Installation of Tabletsat Devices. Details on request.

1

Glavkosmos product — Platform for Installation of the Satellite Tabletsat. Details on request.

1 4

The navigation receiver 14Ц820 is intended for the provision of solving the special-purpose coordinate-time tasks in-the-field.

1 6

Glavkosmos product — Power Module of the Mobile Temperature Control Unit. Details on request.

1 3

Power supply system uses power supply unit for power control in assistance with battery unit for energy storage and up to 14 solar panels as electrical source.

1 10

Pneumatic automation equipment.

1 6

Pneumatic automation equipment.

1 5

Pneumatic automation equipment.

1 5

Pneumatic automation equipment.

1 5

Pneumatic automation equipment.

1 7

Version: thin-film strain gauge pressure sensor, which is a monoblock design with a cable jumper.

1 5

It is made according to "Regulation 98". Version: piezoresistive sensor with a protective metal membrane having flexible, numbered outputs.

1 5

Exception: the strain gage sensor can be supplied with a shock absorber at the request of the consumer. Type of protection - “Sealed enclosure”.

1 5

It is made according to "Regulation 98". Execution: the strain gage sensor at the request of the consumer is made with a screw fitting having a thread M12x1.25 or M18x1.5. Type of explosion protection - ”Sealed enclosure”.

1 5

Version: string converter (SC) and amplifier (A) connected by an integral cable jumper 0.5 m long. Cable jumper sheath TKR tube or steel 12X18H10T (depending on order). Explosion protection type - “Tight sheath”, cable jumper - “Intact cable network” or “Tight sheath” (depending on order).

1 5

Version: strain gauge sensor with cable jumper. At the request of the customer (in the absence of temperature control of the sensor on the product) it is manufactured with a heat-receiving sleeve. The type of explosion protection of the sensor is “Tight sheath”, cable jumper - “Intact cable network”

1 5

Version: thin-film strain gauge sensor with cable jumper. At the request of the customer (in the absence of temperature control of the sensor on the product) it is manufactured with a heat-receiving sleeve. The type of explosion protection of the sensor is “Tight sheath”, cable jumper - “Intact cabl

1 5

Propellant - hydrazine. The unit consists of 2 pressure stabilizers, 6 small-size solenoid valves that supply propellant to the thruster, and two pressure transducers to monitor propellant pressure. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of M

1 6

It is made according to "Regulation 98". Version: strain gauge sensor. The original structural unit and the use of special assembly methods allow you to shift the start of measurement to the level required by the customer. The sensor has a sealed design. Type of protection - “Sealed enclosure”.

1 5

It is made according to "Regulation 98". Exception: potentiometric transducer. The connection between the measurement object and the transducer is carried out using a rope.

1 5

The Software Complex consists of three modules. The Complex is designed for converting digital geodata from standard raster formats into a unified light tile format for data presentation, as well as for monitoring the results of re-conversion, on-line visualization and managing the total amount of d

1

The Program complex is intended for operational visualization of various geospatial information in near real time, as well as for solving a number of basic computing tasks based on it.

1 1

PMA is intended for propellant supply to stationary plasma thrusters. It provides an outlet flow rate of not less than 35 mg/s. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months

1 10

Glavkosmos product — Propulsion System [PS] for Nanosatellite Platform. Details on request.

1 10

One-degree-of-freedom electromechanical device for rotation of spacecraft propulsion thrusters.

1 10

Explosion-proof pumping station with submersible pump.

1 6

Component of the separation device.

1 5

HF element of the antenna feed system paths.

1 2

ERS small-size multiband SAR, intended for operation aboard aircraft of different types. Mathematical, algorithmic and software.

1 4

PMT-187 has bialkali photocathode and 15-cascade secondary-electronic amplifier with mesh dynodes. The input window is made of boron-silicate UV glass, the first dynode is of “proximity” type.

1 10

Glavkosmos product — Radiation Hard Photomultiplier of High Immunity to Magnetic Fields 1. Details on request.

1 10

2/3" Vidicon LI501-1MK target is based on CdSe. Vidicon has magnetic focusing and electrostatic deflection.

1 10

Passive device with the discharge of heat into space.

1 4

As a result, the customer receives a specialized software and hardware VLSI SoC. VLSI may be the only solution that meets the requirements for use in radiation-resistant equipment of critical use.

1 4

Receiving antenna, transmitting antenna, feede

1 3

Modification of the RD120 liquid rocket engine with afterburning of oxidizing gas for the upper stages. Fuel: oxygen + kerosene. A number of new technologies are widely used in engine design. The basic engine RD-120 was developed in 1976-1985. The first launch of the Zenit launch vehicle with the RD

1 8

Liquid rocket engine with afterburning of oxidizing gas. Fuel: oxygen + kerosene. The most powerful liquid rocket engine in the world. More than 1000 fire tests were carried out with a total operating time of more than 110,000 s. During fire tests, engine performance was demonstrated in a wide range

1 8

Liquid rocket engine with afterburning of oxidizing gas. Fuel: oxygen + kerosene. Winner of the competition for the development and supply of the engine for the first stage for the PH of the Atlas family of the American company ULA. More than 260 tests were carried out with a total operating time of

1 8

Liquid rocket engine with afterburning of oxidizing gas. Fuel: oxygen + kerosene. The engine has the widest range of thrust regulation from 105-30%.

1 8

Modification of the RD120 liquid-propellant rocket engine with afterburning of oxidizing gas for the first stages. Fuel: oxygen + kerosene. A number of new technologies are widely used in engine design. The development of the RD182 engine is a terrestrial modification of the RD120MS with a short noz

1 8

Reaction wheels block contains four reaction wheels and provides work of three-axis orientation and stabilization system. Installation into CubeSat platforms provided. Reaction wheels dimensions: diameter 49 mm, width 12 mm, moment of inertia 150 g*cm2.

1 7

Rechargeable battery for power supply of ground infrastructure.

1 9

Rechargeable battery for power supply of spacecraft.

1 9

Glavkosmos product — Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure. Details on request.

1 9

Component of the Ku-band multiple-beam antenna.

1 7

Two-degree-of-freedom electromechanical device for transferring the reflector boom from the transportation to the operational position and for antenna reflector pointing after its deployment.

1 10

Electromechanical device based on linear drives, which is designed to adjust reflective surface profile of the large reflector.

1 10

Component of the C-band antenna which forms planimetric directional diagram.

1 6

Component of the large Ku-band antenna system with planimetric directional diagram.

1 6

Two-degree-of-freedom electromechanical device for transferring the reflector boom from the transportation to the operational position and for antenna reflector pointing after its deployment.

1 10

Monoblock equipment for regulation and monitorung of the spacecraft’s power supply system. It is possible to change the design of the monoblock to increase power up to 10 kW by layout of internal submodules. It is planned to operate as part of a spacecraft for fundamental scientific space research.

1 9

Component of the hold-down system locks of the mechanical device.

1 7

Component of the hold-down system locks of the mechanical device.

1 7

Glavkosmos product — Retractable Mast Mechanism. Details on request.

1 9

Compact four-reflector "Pyramid" retroreflector for onboard calibration on the Condor-FKA satellite.

1 4

Interference-coated angle-reflector panel for laser ranging on the Luna-Globe lander/orbiter.

1 4

Seven-reflector retroreflector array for precision laser ranging of the ESA Sentinel-3 spacecraft.

1 5

36-reflector ring panel for metrological control and calibration of the GLONASS-K2 navigation constellation.

1 5

The receiving single-mirror antenna system includes an antenna with a reflector of 2.5 m with an S-band irradiating system, a slewing ring with electromechanical drives. The structure includes a low-noise input structure of the S-band.

1 7

Training complex for receiving radiosignals of spacecraft.

1 3

Satellite laser ranging and velocity measurement system of spacecraft. It defines the distance considering the delay of reflected laser beam. Velocity measurement is carried out by means of doppler frequency at optical carrier. Receiving of 3D object image or its part.

1 6

Satellite multiband imaging system consist of two identical multispectral camera devices made in the form of separate structural units.

1 9

Assembled, verified and fully tested by the manufacturer satellite platform CubeSat 1U. Payload integration is possible before tests.

1 10

Assembled, verified and fully tested by the manufacturer satellite platform CubeSat 3U. Payload integration is possible before tests.

1 10

Assembled, verified and fully tested by the manufacturer satellite platform CubeSat 3U. Payload integration is possible before tests.

1 10

Assembled, verified and fully tested by the manufacturer satellite platform CubeSat 6U. Payload integration is possible before tests.

1 10

Screen-vacuum thermal insulation (SVTI) is one of the most common and reliable means of passive thermal control in the system for ensuring the thermal regime of a spacecraft. The use of SVTI provides the opportunity to significantly reduce the heat transfer rate of the structural elements and equipm

1

Version: monoblock, including a primary inductive converter and a gain unit. The sensor is tight. Permissible leakage is not more than 1.33 · 10-8 W (1 · 10-4 l · μm Hg / s). Type of protection - “Sealed enclosure”.

1 5

Version: forced-cooling piezoelectric sensor, consisting of a sensor installed in the housing and a flexible cable. Type of protection - “Intrinsically safe electrical circuit” - is provided by an intermediate converter.

1 5

Version: piezoelectric sensor, consisting of a sensor installed in the housing, and a flexible cable. Type of protection - “Intrinsically safe electrical circuit” - is provided by an intermediate converter.

1 5

Component of the separation device.

1 5

Glavkosmos product — Set of Fixing Devices of Nanosatellite. Details on request.

1

Shaping telescopic element in the design of a large transformable reflector.

1 3

Uses Si photo-electric converters and has built-in electromagnetic coils. There is a 13 mm diameter aperture at the panel center with M2 mount holes for sun sensors or payloads.

1 10

Uses Si photo-electric converters and has built-in electromagnetic coils.

1 10

The FAM signaling device includes the following blocks and nodes: optical block, power supply, control unit, PMT block, pulsed light source, flow limiter, set of mounting parts. Since 2009, at the Vostochny spaceport as part of the compressor station.

1 6

Bellows is a thin-wall metal pipe with corrugated (undulated) lateral surface. The bellows are manufactured of: alloy grade "36НХТЮ", beryllium copper grade "БрБ2", stainless steel 12Х18Н10Т, and brass grade "Л-80". Over 200 typical products are manufactured.

1

Electromechanical rotary drive for deployment of large mechanical system elements.

1 8

Glavkosmos product — Single-actuation Drive. Type 2. Details on request.

1 7

Electromechanical rotary drive for deployment of large mechanical system elements.

1 8

Electromechanical rotary drive for deployment of large mechanical system elements.

1 7

Glavkosmos product — Single-Actuation Drive. Type 5. Details on request.

1 8

Electromechanical rotary drive for deployment of large mechanical system elements. With an angular position sensor.

1 8

Component of the mirror antenna. The main function of mirror antennas with a feed of this type is forming a narrow field pattern and repointing the antenna within the specified servicing area if required.

1 5

Glavkosmos product — Single-part and Small-scale Production of Ceramic Modules. Details on request.

1 3

Glavkosmos product — Single-part and Small-scale Production of Interconnection Ceramic Printed Circuit Boards. Details on request.

1 3

Precise and reliable gyroscopic device for measuring the angular coordinates of boreholes, including horizontal drilling, on the basis of fiber-optic gyroscopes and micromechanical accelerometers, which does not require the lifting of drill pipes and preinsertion in the borehole.

1 4

Determination of current coordinates, ground speed and course of traffic with help of space navigation systems(SNS) GLONASS and GPS , solution of service tasks, angle calculation , remembering of individual points and traffic routs, display current location on the map.

1 6

The small-size block for measuring the angular velocity is designed to measure the integrals of the absolute angular velocity vector projections of the spacecraft when operating in the orbital section of the spacecraft as part of the spacecraft control system. The instrument is designed as a free-fo

1 9

An upgraded version for KIND34-040. The small-size device for measuring the angular velocity is designed to measure the integrals of the absolute angular velocity vector projections of the spacecraft when operating in the orbital section of the spacecraft as part of the spacecraft control system. Th

1 9

Electromechanical solar array drive mechanism. Operating regime: continuous rotation.

1 8

Electromechanical solar array drive mechanism. Operating regime: continuous rotation

1 8

Electromechanical solar array drive mechanism. Operating regime: continuous rotation.

1 8

Electromechanical solar array drive mechanism. Operating regime: continuous rotation.

1 8

Electromechanical solar array drive mechanism. Operating regime: continuous rotation.

1 8

Electromechanical solar array drive mechanism. Operating regime: continuous rotation.

1 8

Deployable solar arrays providing up to 25 kW of power for all types of spacecraft.

1 6

The solar cell battery for CubeSat type spacecraft. Solar cell battery is the main element of power supply system, as well as a component part of a measurement and motion control complex satellite system.

1 2

Glavkosmos product — Solar Element GaInP2 / GaAs / Ge. Details on request.

1 6

Platform for testing the solar panel opening mechanism.

1 4

Component of the solar array mechanical device.

1 6

An automated system for weighting large-sized elements of spacecraft - solar panels.

1 6

Single-stage, multi-starting, normally closed, teflon seal Solenoid Valves.

1 9

Single-stage, multi-starting, normally closed, teflon seal Solenoid Valves.

1 9

Single-stage, multi-starting, normally closed, teflon seal Solenoid Valves.

1 9

Single-stage, multi-starting, normally closed, teflon seal Solenoid Valves.

1 9

Single-stage, multi-starting, normally closed, teflon seal Solenoid Valves.

1 9

Platform for small spacecraft weighing up to 180 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separ

1 7

Platform for small satellites weighing up to 70 kg. the Height of the orbit is 1500 km.

1 7

Platform for small spacecraft weighing up to 700 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separ

1 9

On-board digital television system with up to 8 monoblock cameras and an onboard data recording/processing unit.

1 13

High-precision orientation and stabilization system for medium-orbit spacecraft with moments of inertia from 100 to 5000 kg·m². Made on the radiation-resistant element base of Russian rocket and space industry production

1 12

Mechanical device that consists of locks, spring-loaded pushrods, clamp-band with explosive pins, separation connectors, separation sensors.

1 7

Glavkosmos product — Special Transportation Vehicle with a Container. Details on request.

1 3

Glavkosmos product — Spectrometric Photomultiplier Tube. Details on request.

1 8

Glavkosmos product — Spectrometric Photomultiplier Tube 1. Details on request.

1 8

Glavkosmos product — Spectrometric Photomultiplier Tube 1-1. Details on request.

1 8

Glass retroreflector spherical satellite, consisting of two hemispherical menisci and a glass ball.

1

Passive HF device of flight communication equipment.

1 4

Passive HF device of flight communication equipment.

1 4

Glavkosmos product — Star Tracker GEO. Details on request.

1 10

Glavkosmos product — Star Tracker LEO. Details on request.

1 10

Glavkosmos product — Starry Sky Simulator. Details on request.

1 3

Propellant - hydrazine. The unit consists of two modified thermocatalytic thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturing le

1 3

Propellant - hydrazine. The unit consists of two thermocatalytic thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturing lead time i

1 3

Thruster with a discharge power of up to 25 kW. Propellant - xenon. Development status – engineering model. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and eight external magnetic coils. Outside diameter of the accelerating channel is 230 mm

1 10

Thruster with a discharge power of up to 5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system of armored type with magnetic screens. Outside diameter of the accelerating channel is 140 mm. Mean diameter of the accelerating channel is 120 mm. Manu

1 10

Thruster with a discharge power of up to 6 kW. Propellant - xenon. Development status – laboratory model. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens. Outside diameter of the accelerating channel is 140 mm. Mean diameter of the accelerating

1 10

Thruster with a nominal discharge power of 1350 W. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 100 mm. Mean diameter of the accelerating ch

1 10

Version: strain gauge pressure transmitter, which is a monoblock design with a cable jumper.

1 5

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

1 3

CubeSat 1U structure designed in accordance with CubeSat Design Specification rev.13 and supports modular satellite construction based on PC104 PCB stack with solar panels on the edges. For container launches there is a deployment system which consists of 2 separation springs and double separation s

1 7

CubeSat 3U structure designed in accordance with CubeSat Design Specification rev.13 and supports modular satellite construction based on PC104 PCB stack with solar panels on the edges. For container launches there is a deployment system which consists of 2 separation springs and double separation s

1 7

Sun Sensor is a two orthogonal axes digital sun sensor. It generates the directional cosines of the angles of the direction to the sun, thus, it doesn’t require any calibration. Besides, the sun sensor’s size and weight are very small, as is his power consumption which is ultra-low.

1 8

Glavkosmos product — Sun Simulator (halogen). Details on request.

1 6

Full rotary slewing ring with azimuthal elevation drive system with high travel speeds.

1 5

Three-axis full-swing slewing ring with azimuthal elevation drive system and additional tilt axis.

1 7

Operation princicple is based on the use of two independent high-speed channels of the tested product's surface illumination - the object channel (CO) and the background channel (CF).

1 6

Spacecraft are mounted on LV using quick-disconnect devices (locks, pyro-bolts, etc.) that release the spacecraft from the mount after the end of the last stage engine. Remaining free, the spacecraft can hit the detached part. To prevent this, the spacecraft separation system includes exciters (push

1

Glavkosmos product — Technical Condition Monitoring System. Details on request.

1 3

Temperature-controlled honeycomb panels with aluminium face sheets, fixed or attachable heat transfer tubes or fluid loops. Off-the-shelf efficient solutions include standard series of honeycomb fillers and face sheets, filling blocks; possibility of installing heat transfer tubes or fluid loop tube

1 5

Glavkosmos product — Test Bench for Mutual Movement of Spacecraft. Details on request.

1 6

Glavkosmos product — Test Bench For Nanosatellite Attitude Control System. Details on request.

1 3

The mechanism is used in the testbed for testing antenna radio engineering performance in the ground conditions. Development of space version on the base of this solution is available.

1 9

Constructor for assembling nanosatellites from 1U to 12U of the CubeSat form-factor. Dimensions of modules for assembling 100х100х100 mm. Determination of position in space using the optical sensor, GPS/GNSS. Management of M-frames and gyrodyne The stage of manufacturing prototypes and conducting au

1 10

Nonablative thermal-protection silica-fiber-reinforced materials for coating the reusable spacecraft (TZMK-10(М) and TZMK-25(М), as well as radio engineering-purpose articles (TZMK-14М).

1 5

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a nozzle, a propellant injection unit, two small-size solenoid valves that supply propellant to the thruster, and a pressure signaling indicator that monitors the fact that the thruster

1 10

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a nozzle, a propellant injection unit, two small-size solenoid valves that supply propellant to the thruster, and a pressure signaling indicator that monitors the fact that the thruster

1 9

Version: thermoelectric converter (TC) consists of a sensitive element placed in the housing, a cable jumper and a connector. The sensitive element is based on a thermocouple cable with mineral insulation TU 16-505.757.

1 5

Consists of two units: M-70 Stationary Plasma Thruster and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).

1 10

TCM is a metal structure, which consists of a basement and a rotary frame. Hydraulic and electric equipment for the frame lifting / lowering is placed inside the basement. Electric cables run along the rotary frame. On top of the frame a couplers-removing mechanism is placed.

1

Automated weightlessness system of large-sized elements of spacecraft.

1 4

In accordance with the specification of the customer.

1 4

The eqiupment structually consists of: - Transport Unit tow-truck ; - Semi-trailer; - Special tank-container.

1 3

The station includes an antenna system with a reflector of 7.2 m Ku-band. The design of the reflector is collapsible. The structure includes an antenna on a folding slewing ring, a thermal container with a guidance system and channel-forming equipment.

1 9

Transportable navigation equipment 14Ц821 is designed to be used in equipment of motor-vehicles and armored machinery with the aim of solution of special coordinate-timing tasks.

1 6

Contains:Temperature control module, ventilation module, control module and power supply module of 2 modern diesel power generators.

1 4

The Transporter-Erector consist of a rigid metal frame, mounted on special railway carriages; a boom with the supports and special devices for ILV placing and transportation, assembled on the fame; hydraulic cylinders for boom erection into upright position and provision of ILV placing on launch pad

1 4

Assembled on Transporter-Erector frame pipe connector unit with mating device, providing mating with pipe connectors of Launch Complex, Assembling and Testing Facility, T.-E. depot.

1 4

Propellant - hydrazine. The unit consists of one modified thermocatalytic low thruster. Thermal mode of the unit is ensured by 2 heaters (1 main and 1 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 3 temperature sensors. Manufacturing lead time is given without t

1 3

Propellant - hydrazine. The unit consists of three modified thermocatalytic low thrusters. Thermal mode of the unit is ensured by 3 heaters (2 main and 1 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 3 temperature sensors. Manufacturing lead time is given withou

1 3

Structurally the Device composition is as follows:

1 3

Two-degree-of-freedom electromechanical device for antenna pointing.

1 8

Two-degree-of-freedom electromechanical device for antenna pointing.

1 8

Two-degree-of-freedom electromechanical device for antenna pointing.

1 8

Two-degree-of-freedom electromechanical device for antenna pointing.

1 8

Antenna deployment occurs by burning the filament. The device for burning the filament is duplicated. Telemetry monitoring of antenna deployment is performed.

1 8

Glavkosmos product — UHF Transceiver. Details on request.

1 10

Ultra-black coatings with reflection of non-informational radiation in the spectral range of 0.42-2.5 microns no more than 0.5 – 1.0 % with an active lifetime of 15 years.

1 5

Glavkosmos product — Ultrasound Diagnostic Medical System "RuScan 50". Details on request.

1

Glavkosmos product — Ultrasound Diagnostic Medical System "RuScan 60". Details on request.

1

Glavkosmos product — Ultrasound Diagnostic Medical System "RuScan 65". Details on request.

1

Glavkosmos product — Ultrasound Diagnostic Medical System "RuScan 65M". Details on request.

1

Glavkosmos product — Ultrasound Diagnostic Medical System "RuScan 70P". Details on request.

1

UM is a metal structure, which consists of a basement and a rotary frame (consisting of two frames of different shape). Hydraulic and electric equipment for the frame lifting / lowering is placed inside the basement. Different kind of lines run along the rotary frame. At the top of the frame coupler

1

The unified DC-DC conversion module is included in the set of unified modules for critical power management systems. The set of unified modules for critical power management systems is designed for use in guaranteed power systems for aircraft engines, electric drives for pumping oil, gas, chemical p

1 16

The unified power control and management module is included in the set of unified modules for critical power management systems. A set of unified modules for critical power management systems designed for use in guaranteed power systems for aircraft engines, electric drives pumping oil, gas, chemica

1 19

The Unit provides necessary flow rate, pressure and temperature set by the operator, in the circuit of the Product's liquid fluid temperature control system. Intelligent operation control system. Self-diagnostic system.

1 4

Equipment consists of: - container equipped with two motor-generators; - set of uninterruptible power supplies; - set of low-voltage packaged devices; - remote control and management system.

1 4

Platform for small spacecraft weighing up to 700 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separ

1 7

Platform for small spacecraft weighing up to 700 kg. Height of operation on different types of orbits – from low circular to geostationary. The ICA platform is divided into several independent modules. Each module separately is a subsystem of the platform and is a functionally and structurally separ

1 7

Modular platform for small spacecraft for various purposes, for all types of orbits.

1 6

Modular spacecraft platform for all types of orbits.

1 6

In accordance with the specification of the customer. On the basis of the basic upper stage "Fregat" a number of highly efficient booster blocks have been created. The use of additional fuel tanks and a dropable block of tanks (upper stage "Fregat-MT" and upper stage "Fregat-SB") at upper stage "Fre

1 8

DRT-LSN, together with ORTD-LSN, is intended for use in the equipment of base stations and subscriber terminals of the local navigation system. Separately, DRT-LSN VLSI can be used as a microcontroller for universal use. The microcircuit is intended for use as part of the subscriber module of the LA

1 10

Glavkosmos product — VLSI 16-bit ADC with a Sampling Frequency of 200 MHz. Details on request.

1 13

Silicon-germanium BiKMOS VLSI broadband quadrature demodulator is designed for use in radio paths of military and special equipment and provides:

1 12

Silicon-germanium BiCMOS VLSI frequency synthesizer based on direct digital conversion is designed to produce a stable high-frequency signal in the 600 MHz range with an ultra-low frequency tunning step, low phase noise and fast frequency tunning, as well as the possibility of frequency, phase and L

1 14

VLSI kit for low-power GLONASS / GPS navigation receiver.

1 10

The microcircuit of the "System in the case" type (SIC) is intended for use in civil navigation equipment. It receives and processes GNSS signals: GLONASS L1OF, L1OC; GPS C/A L1; GALILEO E1B, E1C; as well as SBAS L1, DCMS L1OC and solutions to the navigation problem.

1 10

Semi-order programmable VLSI central computers are designed to create on their basis a new generation of integrated flight control systems (IFCS) of manned and unmanned aerial vehicles using heterogeneous communication channels. VLSI provide the design based on these circuits of the required functio

1 7

Silicon-germanium BiKMOS VLSI broadband quadrature modulator is designed for use in radio paths of special equipment and provides:

1 11

Current and voltage regulator for spacecraft onboard equipment. Is designed to provide spacecraft with electricity. Converts 110-180 V DC to 28,5 V DC. Voltage converter with other input/output voltage values can be built based on this design.

1 8

Current and voltage regulator for spacecraft onboard equipment. Is designed to provide spacecraft with electricity. Converts 28,5 V DC to 120 V DC. Voltage converter with other input/output voltage values can be built based on this design.

1 8

The voltage converter for onboard equipment of the spacecraft. Provides stable high-precision AC power for a single-phase network of spacecraft onboard equipment. Features: - output voltage frequency 1000 Hz POS 80 RNM is an upgraded voltage converter. It is designed to replace POS 80 RN voltage con

1 7

Elements of antenna feed system and flight communication equipment paths of different frequency bands.

1 7

Structurally the Device UVDR-1200 composition is as follows:

1 3

Structurally the Device composition is as follows:

3

Structurally the Device UVR-200 composition is as follows:

1 3

Welded steel diaphragm bellows are unique products consisting of annular diaphragms with desired pattern, connected in series between each other by welding on the outside and inside diameter.

1

Hydrazine storage and feed to liquid propellant thrusters

1 9

Glavkosmos product — X-band Transmit/Receive Antenna. Details on request.

1 7

The X-band transmitter designed for the lunar spacecraft (Luna-25 lander and Luna-26 orbiter). Сertified for compatibility with ESA ground stations.

1 8

The Cubesat X-band Transmitter with high throughput up to 1 Gbps.

1 7

Propellant – xenon, nitrogen. The thruster components are: a thermal accumulating chamber with a heater and a nozzle installed on it, two small-size solenoid valves that supply propellant to the chamber, and MLI. The thruster also has electrical connectors and a mounting plate that joins the thruste

1 10

Pneumatic automation equipment.

1 6

Pneumatic automation equipment.

1 6

Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the required distribution of the propellant flow rate. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procu

1 2

Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the required distribution of the propellant flow rate. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procu

1 2

Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the required distribution of the propellant flow rate. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procu

1 2

Consists of a flow regulator that regulates the total flow rate; anode and cathode restrictors that ensure the required distribution of the propellant flow rate. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procu

1 2

Consists of two xenon flow controllers. Propellant - xenon. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).

1 6

Compact star tracker designed for small spacecraft (nano- and micro-satellites).

1 7

The functional purpose of VLSI is the coordinated filtering and compression of FM and LFM weak signals with a base of 4096 or more. The use of VLSI SF in devices for secondary processing of weak signals allows to increase the detection range of targets while maintaining high resolution and allows th

1 14

Launch Slots

1
Soyuz 2.1b/Fregat-M
LO Available
Soyuz 2.1b/Fregat-M
31 Dec 2027
Vostochny Cosmodrome, Siberia, Russian Federation
Log in to request

Reviews

No reviews yet — reviews come only from verified buyers after a completed request.

Write a review

0 / 2000
← All providers