Space Hardware Marketplace

ChallengeOne Power Supply System (PSS/EPS)

• Input voltage5-14 V
• PV panel channels3
• PV panel typeGaAs, Si

Electrical power system module for the ChallengeOne satellite platform with 3 solar-panel channels (GaAs/Si), battery charging and 4…

ChallengeOne On-Board Computer (OBC)

• Input voltage5-14 V
• Communication bus2x CAN2B; Raspberry Pi camera interface; UART; I2C; SPI (2 CS); USB
• Operating temperature-40 to +85 °C

Onboard computer module for the ChallengeOne satellite platform with dual CAN2B buses, Raspberry Pi camera interface and UART/I2C/SPI/USB…

ChallengeOne Transceiver Module

• Input voltage5.5 - 20.0 V
• Frequency band150 to 960 MHz
• Antenna interface impedance50 Ohm

VHF/UHF-band transceiver module for the ChallengeOne satellite platform, supporting up to +33 dBm output over CAN/USB/I2C/SPI interfaces.

ChallengeOne SDR Module

• Input voltage5.5 - 20.0 V
• Frequency band1 kHz to 2 GHz
• Antenna interface impedance50 Ohm

Software-Defined Radio module for the ChallengeOne satellite platform, covering 1 kHz to 2 GHz over a USB 2.0…

ChallengeOne LoRa Gateway Module

• Input voltage5.5 - 18.0 V
• Frequency bandsubGHz
• Antenna interface impedance50 Ohm

Space-qualified LoRa (Long Range) gateway payload module for the ChallengeOne satellite platform, receiving low-bandwidth IoT telemetry from ground…

ChallengeOne CubeSat Platform

• Orbit altitude550 km (LEO)
• Orbital velocity7.5 km/s
• Orbital period90 minutes

Configurable nanosatellite/kit-satellite platform developed by Telnet for LEO IoT-gateway missions; flight-proven on the ChallengeOne mission (Tunisia's first satellite).

Teledyne e2v CCD201-20 Electron Multiplying CCD (EMCCD)

• Active pixels1024 x 1024
• Pixel size13 µm square
• SensitivitySingle photon sensitive

Frame-transfer electron multiplying CCD (EMCCD) designed for extreme performance in high frame rate, ultra-low light applications, with single-photon…

Teledyne e2v CCD97-00 Compact Electron Multiplying CCD (EMCCD)

• Active pixels512 x 512
• Pixel size16 µm square
• SensitivitySingle photon sensitive

Compact frame-transfer electron multiplying CCD sensor designed for extreme performance in high frame rate, ultra-low light applications such…

Teledyne e2v CCD230-84 Large-Area Back-Illuminated Scientific CCD

• Number of pixels4096 (H) x 4112 (V)
• Pixel size15 µm square
• Image area61.4 mm x 61.4 mm

Large-area, back-illuminated scientific CCD image sensor for low-noise spectroscopy and broadband scientific imaging applications.

Teledyne e2v CCD351-00 L3Vision Electron Multiplying CCD

• Active pixels1024 x 1024
• Pixel size10 µm square
• GainVariable multiplication gain, 1x-1000x+

Frame-transfer L3Vision electron multiplying CCD sensor designed for extreme performance in high frame rate, ultra-low light applications, with…

Teledyne e2v CCD290-99 Large-Area Back-Illuminated Scientific CCD

• Number of pixels9216 (H) x 9232 (V)
• Pixel size10 µm square
• Image area92.2 mm x 92.4 mm

Large-area, back-illuminated scientific CCD image sensor for demanding astronomical and scientific imaging applications, with very low read-out noise…

Teledyne e2v CCD47-20 Frame-Transfer Scientific CCD

• Image format1024 by 1024 (1:1)
• Image area13.3 x 13.3 mm
• IlluminationFront or back illuminated format

Frame-transfer CCD sensor with extremely low noise amplifiers, made with Teledyne Space Imaging's Advanced Inverted Mode process for…

Thermally Conductive Vibration Isolation System (TCVIS)

• FunctionCombined thermal transport (via GFTS graphite fiber strap) and 6-axis active vibration cancellation
• Vibration reduction (axial, drive frequency)> 40 dB (100:1 reduction)
• Vibration reduction (radial, drive frequency)31 - 37 dB (37:1 to 70:1 reduction)

Combined thermal-transport and 6-axis vibration-cancellation assembly for cryocooler-to-detector-dewar interfaces, co-developed with CSA Engineering and tested at NIST.

PyroFlex PGS & Graphene Thermal Straps (X-Series)

• MaterialPyrolytic Graphite Film/Sheet (PGF/PGS), optional Graphene Layered Foil
• Thermal conductivity1,350 - 2,500 W/(m-K), depending on material, temperature, and sheet thickness
• Performance vs. metals6x the performance of aluminum and 4x the performance of copper at room temperature

Ultra-low-stiffness pyrolytic graphite sheet (PGS) and graphene foil thermal straps offering the industry's highest thermal conductivity, NASA JPL…

Graphite Fiber Thermal Straps (GFTS)

Lightweight, high-conductance graphite-fiber flexible thermal links with vibration damping on all 3 axes; the space industry's only carbon-fiber…

Cryocooler Series Thermal Straps (CS-CuTS)

• Material99.99 - 99.998% pure OFHC copper (Cu-101)
• CablingTAI exclusive OFHC UltraFlex I (2.5mm) copper cabling
• Cold head diameters9 (2nd stage) cold head diameters available

Standard copper thermal strap line sized to common Sumitomo (SHI) and Cryomech cryocooler cold-tip diameters, with 72 sub-models…

Copper Cable Thermal Straps (CuTS)

• Material99.99 - 99.998% pure OFHC copper (Cu-101)
• CablingTAI exclusive OFHC UltraFlex I (0.10 in / 2.5 mm) and UltraFlex II (0.20 in / 5 mm) copper cable
• Standard models127 standard models, plus Cryocooler Series (72 sub-models)

OFHC copper-cable flexible thermal links used to passively conduct heat between spacecraft and cryogenic components, offered in 127…

SAUDIGEOSAT-1 (SGS-1)

Ka-band High Throughput Satellite built for KACST and operated by Taqnia Space at 39°E, delivering secure aero, maritime,…