Sputnix

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29 Products

15 Years Active

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About Sputnix

Sputnix LLC is a Russian private space company founded in 2011 and headquartered in Moscow, developing CubeSat platforms, spacecraft subsystems, and space engineering educational kits for commercial, research, and educational customers. The company produces the SXC3 3U CubeSat satellite bus, the OrbiCraft-Pro educational CubeSat kit designed for hands-on space engineering training, and deployable antenna systems for small satellites. Sputnix is recognised as one of Russia's first commercial CubeSat manufacturers and has contributed to the development of Russia's private NewSpace sector by making accessible, flight-proven small satellite hardware available to universities, research institutes, and commercial operators.

Company Info

Headquarters Moscow, Russia, Russia

Founded 2011 (15 years)

Specializations

manufacturer

Website sputnix.ru ↗

Email info@sputnix.ru

Photos 5

Products

Hardware-in-the-loop simulation bench for developing and verifying attitude determination, stabilization and navigation systems of small spacecraft under conditions emulating LEO flight (Helmholtz/Merritt coil magnetic field, air-bearing, sun simulator, optical tracking). Available in three configurations from CubeSat (01) to educational (02) to professional small-satellite testing (03).

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Type	ADCS hardware-in-the-loop bench —
SXC config 01	CubeSat 1U/3U/6U; Helmholtz coils 2 m, Ø600 mm uniform field; air-bearing ≤ 35 kg; pointing accuracy ≤ 0.25° —
SXC config 02	Educational; Helmholtz coils 1.3 m, Ø250 mm field; air-bearing ≤ 35 kg; accuracy ≤ 1° —
SXC config 03	Professional small-sat; Merritt coils; Ø900–1300 mm field; air-bearing ≤ 160 kg; accuracy ≤ 0.3° —
Sun simulator	≥ 90,000 lx at 1.5 m, ~6000 K —
Magnetic field amplitude	± 150 µT (config 01) —
Variants	SXL-SCOE-ADCS-01 / -02 / -03 —

Debug/development tools for OrbiCraft-Pro payloads: the SXC-MBB-03 payload base board for SXC1/SXC3 platforms (design & software released by SPUTNIX as open source), and the SXC-DEVKIT-06-BG payload developer kit for SXC6 (functional testing of platform components, the board stack and payload-compatibility work).

1 4

Type	Payload development & debug tools —
SXC-MBB-03	Payload base board for SXC1 / SXC3 (open-source design & SW) —
SXC-DEVKIT-06-BG	Payload developer kit for SXC6 —
Use	Component & board-stack functional tests, payload compatibility —

Mission Control Center for centralized, automated control of a spacecraft or satellite constellation in Earth orbit. It aggregates data from all ground stations, then processes, analyses and stores the incoming information and issues commands.

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Type	Mission Control Center (software & facility) —
Function	Centralized automated control of spacecraft / constellations —
Inputs	Aggregates telemetry from all ground stations —
Operations	Data processing, analysis, storage and commanding —

1U CubeSat satellite platform / assembly kit. The "Flight" (SXC1-GA) version is factory-assembled and tested with GaAs solar panels, ready for payload integration; an "Experimental" (SXC1) lab/educational version is also offered.

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Form factor	1U CubeSat —
Dimensions	108 × 108 × 113.5 mm
Mass (without payload)	≤ 0.95 kg (GaAs)
Max mass (with payload)	≤ 1.33 kg
Payload volume	80 × 70 × 20 mm
Solar cells	6 (GaAs / Si) —
Battery	Li-Ion 2S 5000 mAh, ≥ 39 Wh —
Bus voltage	7.4 V nominal
Radio	435–437 MHz, AX.25, up to 9600 bit/s —
ADCS	Electromagnetic, B-DOT detumbling —
Bus interface	CAN 2.0B —
Operating temperature	−30 … +60 °C
Variants	SXC1 (Experimental), SXC1-GA (Flight) —

3U CubeSat satellite platform / assembly kit. The "Flight" (SXC3-GA) version is factory-assembled and tested with GaAs solar panels. Variants: Experimental (SXC3), Flight (SXC3-GA), Pro (SXC3-GA-ADC) with enhanced attitude control.

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Form factor	3U CubeSat —
Mass (without payload)	1.4 kg
Max mass (with payload)	4 kg
Dimensions	108 × 108 × 340.5 mm
Payload volume	80 × 70 × 20 mm
Solar cells	14 —
Battery	Li-Ion 2S 5000 mAh, ≥ 39 Wh —
Bus voltage	7.4 V nominal
Payload power (orbit-avg)	≥ 600 mW
Radio	435–437 MHz, AX.25 / FEC, 4800–56700 bit/s —
ADCS	B-DOT + gyro & magnetometer sensors —
Bus interface	CAN 2.0B —
Operating temperature	−30 … +60 °C
Variants	SXC3, SXC3-GA, SXC3-GA-ADC —

Functional 1U/3U CubeSat training kit with full set of subsystems (OBC, EPS, ADCS, comms) for universities.

1 9

Kit type	Functional CubeSat training kit —
Form factor	1U / 3U —
Mass (1U)	~1.0 kg
Subsystems	OBC, EPS, ADCS, UHF transceiver, structure —
Ground SDR	included —
Power (orbit)	2 W
Battery	Li-Ion 10 Wh —
Use case	Universities, schools, R&D —
Software	Lua-scripted flight SW —

Microsatellite bus for spacecraft of 80–200 kg, providing service systems and accommodation for a wide range of payloads independent of the target-instrument configuration. Designed for high-resolution Earth observation and other LEO missions.

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Platform class	Microsatellite bus, 80–200 kg spacecraft —
Orbit	LEO, 500–800 km
Design lifetime	≥ 3 years
Platform mass (instruments)	≤ 120 kg
Payload mass	≤ 80 kg
Bus voltage	27 V
Solar array power (max)	up to 500 W
Average orbital power	up to 250 W
TT&C (S-band)	1 / 0.5 Mbit/s, CCSDS —
Payload downlink (X-band)	up to 1500 Mbit/s, DVB-S2 —
ADCS	3-axis; pointing ±0.05°, attitude determination ≤ 30″, stabilization ±0.001°/s —
Interfaces	SpaceWire, CAN 2.0B, LVDS —

New-generation CubeSat platform built on SPUTNIX's extensive design, serial-production and operations heritage. Optimized structure offers maximum free payload volume and power, with improved onboard systems. Available in 4U and 16U configurations.

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Form factor	CubeSat 4U / 16U —
Dimensions (16U)	226 × 226 × 454 mm
Bus interface	CAN 2.0B (up to 1 Mbit/s) + CAN-FD (up to 5 Mbit/s) —
TM/TC radio	Redundant, 2400–115200 bit/s, dipole + patch, 401 / 435 MHz —
Variants	SG3 4U, SG3 16U —

Laboratory UHF transceiver for working with satellites in lab conditions over the standard radio channel. Connects to a PC via USB and is controlled by Houston CC software, allowing the frequency to be tuned in software.

1 11

Type	Laboratory UHF transceiver —
Frequency range	398–410, 435–438 MHz
TX output power	10 mW (10 dBm) —
Power at antenna	28 mW
Interface	mini-USB 2.0 —
Antenna	Stick —
Mass (with antenna)	≤ 235 g
Dimensions	149 × 64 × 49 mm
Supply voltage	4.7–5.5 V
Software	Houston CC —
Operating temperature	+15 … +45 °C

Attitude-control actuators of the SX-SBOX suite for microsatellite platforms: ADCS control unit, reaction wheel, magnetorquers and a magnetorquer control unit.

1 5

ADCS control unit SX-SBOX-ADCU-01	ARM Cortex-M4 160 MHz, hot-redundant, RTOS, ≤5 W, 220 g —
Reaction wheel SX-SBOX-RWH-50-2.0-01	Max torque 0.05 N·m, momentum 2 N·m·s, 43 W peak, 3.2 kg —
Magnetorquers SX-SBOX-MTQ	SX-MT-1…SX-MT-30: dipole 1–30 A·m², 200–1200 g —
Magnetorquer control unit SX-SBOX-MTQU-01	3 channels, PWM, ≤2 W/channel, 85 g —
Interface	CAN 2.0B —

Attitude-determination and navigation sensors of the SX-SBOX suite for microsatellite platforms: satellite navigation, GNSS antenna, MEMS and fiber-optic angular-rate sensors, magnetometer and sun sensor.

1 7

Satellite navigation SX-SBOX-GNSS-01	Position 10 m (σ), velocity 0.01 m/s, 2 W —
GNSS antenna SX-SBOX-AGG-01	1559–1607 MHz, gain ≥5.5 dB, RHCP, 61 g —
MEMS rate sensor SX-SBOX-AVS-MEMS-01	Bias drift 2°/h, noise 0.15°/√h, 0.6 W, 75 g —
Fiber-optic gyro (GIVUS) SX-SBOX-AVS-FOG-01	Bias drift ≤0.005°/h, noise ≤0.0007°/√h —
Magnetometer SX-SBOX-MAG-01	Range ±100,000 nT, noise 100 nT, 70 g —
Sun sensor SX-SBOX-SUNS-01	FOV 45° half-cone, accuracy 0.15°, 45 g —
Interface	CAN 2.0B —

Communications line of the SX-SBOX suite for microsatellite platforms: UHF and S-band command-and-telemetry radio links, X-band high-speed downlink (VRL-X), the high-speed-radio control unit, and UHF/S/X-band antenna-feed systems.

1 6

UHF TT&C SX-SBOX-TRX-UHF-01	435–438 MHz, 5 W, up to 19200 bit/s, AX.25/USP, RX −109 dBm —
S-band TT&C SX-SBOX-TRX-S-01	RX 2025–2110 / TX 2200–2290 MHz, 5 W, up to 10 Mbit/s, LDPC, AES-128/256, CCSDS —
X-band downlink (VRL-X) SX-SBOX-XBOX	8220 MHz, 600–1750 Mbit/s, DVB-S2/S2X, ±65° scan, EIRP 68 dBm, 15 kg —
High-speed-radio control unit	CAN control, RS-422 ×4, 0.75 kg —
Antenna systems	UHF 400–403 MHz (21 g); S-band 2000–2290 MHz ≥4 dB; X-band 8000–8400 MHz ≥22.5 dB —
Interfaces	CAN 2.0B, SpaceWire, Ethernet —

Onboard computing line of the SX-SBOX instrument suite for microsatellite (Pallada-class) platforms: the onboard computer, a SpaceWire router with onboard mass memory, and flight software.

1 6

Family	Onboard computing (SX-SBOX line) —
Onboard computer SX-SBOX-OBC-01	171 × 111 × 51 mm, 0.86 kg, ≤10 W; CAN2B, SpaceWire, MIL-STD-1553 (opt) —
SpaceWire router + memory SX-SBOX-SPW-OBDH-MEM-01	8 MB, up to 16 ports, SpaceWire up to 200 Mbit/s, RMAP (ECSS-E-ST-50-52C) —
Flight software	SX-SBOX-KINOSOFT —
Supply voltage	22–34 V (500 V galvanic isolation) —
Interfaces	CAN 2.0B, SpaceWire —

Electrical-power line of the SX-SBOX suite for microsatellite platforms: the power regulation & control apparatus (PRU) and the power distribution/switching unit (BKP).

1 6

Regulation & control SX-SBOX-PRU-01	306 × 161 × 140 mm, 7 kg, 10 W —
Regulated isolated bus	27 V (ECSS-E-ST-20-20C) —
Unregulated bus	27 V (ECSS-E-ST-20-20C) —
Power distribution unit SX-SBOX-PDU-HI-01	244 × 171 × 45 mm, 1.1 kg, up to 8 loads, cold-redundant —
Supply voltage	22–34 V
Interfaces	CAN 2.0B, RS-485, SpaceWire —

Thermal-control line of the SX-SBOX suite for microsatellite platforms: the thermal-control-system control unit (BU-SOTR) and engineering services for topology optimization.

1 7

Thermal control unit SX-SBOX-THERMU-01	200 × 130 × 30 mm, 600 g, ≤5 W (heaters off) —
Redundancy	2 half-sets —
Heater channels	14 per half-set, ≤60 W each —
Temperature sensors	36 analog (P1K0) + 14 digital (DS18B20Z) per half-set —
Topology optimization	SX-TOPOLOGY (engineering service) —
Supply voltage	22–33 V
Interface	CAN 2.0B —

OrbiCraft-Pro reaction wheel assembly — a complete set of attitude-control actuators comprising four reaction wheels with drivers and control electronics, for nanosatellite attitude determination and control systems.

1 11

Type	4-wheel reaction wheel assembly (with drivers & electronics) —
Dimensions	97 × 97 × 80 mm (<1U) —
Mass	520 g
Supply voltage	4–15 V
Power consumption	2–8 W (at 2000–6000 rpm) —
Speed range	± 6000 rpm (up to ±10000 rpm on request) —
Max torque (X/Y/Z)	9.1 / 9.1 / 4.7 mN·m
Angular momentum (@6000 rpm, X/Y/Z)	±18 / 18 / 9.6 mN·m·s
Data interface	CAN 2.0B —
Operating temperature	−30 … +85 °C
Qualification	QT / AT (functional, vibration, shock, thermal-vacuum) —

Onboard computer (OBC) for satellite control, with a Raspberry CM3 processor slot, an autonomous attitude-control (ADCS) microcontroller, sensor suite and magnetorquer drivers. Integrates flight management and B-DOT magnetic attitude control.

1 12

Type	Onboard computer + ADCS controller —
Dimensions (without PC104)	86.2 × 93.6 × 14 mm —
Mass	55 g
Supply voltage	5–14 V
Power consumption	0.25 W (sensors) / 0.9 W (with Raspberry Pi) —
Main processor	Raspberry CM3, quad-core ARMv8 up to 1.2 GHz, 4 GB flash, 1 GB RAM —
ADCS MCU	80 MHz, 2 MB flash, 128 KB RAM —
Magnetorquer drivers	3 channels, up to 500 mA each —
Interfaces	CAN 2.0B; Raspberry: Camera I/F, UART, I2C, SPI, USB —
Telemetry	Voltages, currents, magnetometer, angular rate, temperature —
Operating temperature	−40 … +85 °C
Qualification	QT / AT (functional, vibration, shock, thermal-vacuum) —

Electrical power system (EPS) managing satellite power from the SXC-BAT-03 battery pack and up to 14 solar panels. Includes battery heating channels, Remove-Before-Flight inhibits and an economical control microcontroller.

1 12

Type	EPS (power conditioning unit + battery pack) —
PCU dimensions	96 × 89 × 14 mm —
Solar panel channels	3 (GaAs / Si), up to 3000 mA total —
Bus voltage	8 V (from panels) / 6.0–8.4 V (from battery) —
Output channels	4, up to 5000 mA total —
Battery type	Li-Ion / LiFePO4, 2S (5.0–8.5 V) —
Battery capacity	10.6 A·h (39.8 Wh) —
Battery heater channels	2 —
Data interface	CAN 2.0B, UART —
Telemetry	Input/output voltages & currents, battery state, temperature —
Operating temperature	−40 … +85 °C
Qualification	QT / AT (functional, vibration, shock, thermal-vacuum) —

Sun sensor for nanosatellite attitude determination and control. The CAN interface allows a single sensor or a daisy-chain of sensors; it measures the cosine of the angle to the Sun across a wide field of view.

1 12

Type	Two-axis sun sensor —
Dimensions (without connector)	28 × 23 × 7 mm —
Mass	10 g
Supply voltage	4–14 V
Power consumption	15–25 mW
Interface	CAN 2.0B —
Field of view	± 60° (FOV cone) —
Accuracy	± 0.3° (1σ), ± 0.8° (3σ) —
Noise-equivalent angle	± 0.1° —
Telemetry rate	10–20 Hz
Operating temperature	−40 … +85 °C
Qualification	QT / AT (functional, vibration, shock, thermal-vacuum) —

GaAs (gallium arsenide) solar panels with integrated electromagnetic torquer coils for CubeSat structures. Side version (SXC-SGS-03) mounts on the side edge of a 1U body; end version (SXC-SGE-03) mounts on the end faces of 1U/3U bodies. Multiple panels can be combined.

1 12

Cell type	GaInP/GaAs/Ge triple-junction on Ge substrate —
Cell efficiency	28 %
Dimensions	98 × 82.6 × 8.6 mm (1.7 mm thick without connector) —
Mass	30–34 g
Open-circuit voltage (Voc)	5.3 V
Short-circuit current (Isc)	500 mA
Max-power point	4.7 V / 480 mA —
Integrated torquer coil	1.9 m² equivalent area, 200 Ω —
Interface	Hirose GT8E, scalable —
Operating temperature	−40 … +85 °C
Variants	SXC-SGS-03 (side), SXC-SGE-03 (end) —
Qualification	QT / AT (functional, vibration, shock, thermal-vacuum) —

OrbiCraft-Pro UHF-band transceiver on a PC104 board for the spacecraft electronics stack, with an SMA antenna connector and antenna-deployment interface. Supports AX.25 and USP (FEC) protocols.

1 13

Type	UHF transceiver (PC104 board) —
Dimensions (without PC104)	87 × 93 × 13 mm —
Mass	43 g
Supply voltage	5–14 V
Power consumption	3.5 W (TX) / 0.2 W (RX) —
Operating frequency	434–438 MHz (400–401 MHz option) —
Output power	30–33 dBm (1–2 W, adjustable) —
Modulation	GMSK —
Data rate	2400–57600 bit/s
Receiver sensitivity	−119 dBm
Protocols	AX.25, USP (FEC) —
Interfaces	CAN 2.0B, UART; RF SMA 50 Ω + antenna deployment —
Operating temperature	−40 … +85 °C

Versatile, configurable 12U CubeSat nanosatellite platform of onboard service systems and structural elements, compatible with standard serial 12U deployers. Supports redundant onboard computers and a cold-gas propulsion option for high-accuracy remote-sensing missions.

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Form factor	12U CubeSat —
Dimensions	226.3 × 226.3 × 366 mm
Max mass (with payload)	≤ 24 kg
Battery	Li-Ion, ≥ 120 Wh —
Bus voltage	6.0–8.4 V
Solar power (peak, LEO)	≥ 50 W
Service radio	400–401 MHz, USP+FEC, up to 57600 bit/s —
Payload downlink (X-band)	8–8.4 GHz, up to 100 Mbit/s, DVB-S2 —
ADCS	B-DOT, sun/nadir/target pointing; gyro, magnetometer, sun & star sensors —
Pointing accuracy	up to 0.1° (imaging stabilization up to 0.01°) —
Propulsion	Cold-gas correction thruster —
Operating temperature	−30 … +60 °C
Design lifetime	≥ 1.5 (up to 3) years

Versatile, configurable 6U CubeSat nanosatellite platform of onboard service systems and structural elements. Accepts third-party payloads compliant with the SXC6 ICD. Modifications: SXC6-VOL (Basic, max payload volume), SXC6-ADC (with ADCS), SXC6-RS (remote sensing).

1 15

Form factor	6U CubeSat —
Dimensions	118.6 × 228.6 × 366 mm
Mass (without payload)	≤ 3.4 kg
Max mass (with payload)	≤ 12 kg
Battery	Li-Ion 2S, ≥ 78 Wh —
Bus voltage	6.0–8.4 V (7.4 nominal) —
Solar power (per cell, LEO)	≥ 15 W
Radio	435–438 MHz, AX.25 / USP+FEC, up to 57600 bit/s —
Transmitter / receiver	TX ≥ 30 dBm / RX −113 dBm —
Antenna	Patch, 3 dBi —
ADCS	B-DOT + gyro & magnetometer sensors —
PC interface	micro-USB, WiFi —
Bus interface	CAN 2.0B —
Operating temperature	−30 … +60 °C
Variants	SXC6-VOL, SXC6-ADC, SXC6-RS —

Anechoic chamber for testing spacecraft transceiver chains, antenna-pattern measurement, EMC testing and other purposes. Operates from 200 MHz to 45 GHz and is mobile, with a radio-transparent test table.

1 9

Type	Mobile anechoic (EMC) chamber —
Frequency range	0.2–45 GHz
External dimensions	≥ 2 × 2 × 2 m
Anechoic volume	0.7 × 0.7 × 0.7 m
Door opening	≥ 1.9 × 1.9 m
Anechoic performance	≥ 20 dB (400–440 MHz) —
Shielding	≥ 40 dB (400–440 MHz) —
Absorber pyramid height	350 mm
Features	Mobile; radio-transparent test table —

Air table for testing relative motion of spacecraft: a precision aluminium horizontal surface with an even grid of holes providing near-frictionless free motion of test objects in the horizontal plane (air-cushion pucks).

1 8

Type	Air-bearing relative-motion table —
Overall dimensions	5000 × 4000 × 3000 mm
Active area	1860 × 2480 mm
Puck payload capacity	up to 10 kg
Puck-to-table gap	≤ 0.5 mm
Working medium	Air —
Surface levelling accuracy	≤ 0.1 mm
Independent measurement	≤ 1° attitude, ≤ 10 mm position —

Bench for calibration and verification of small matrix and diode-type sun sensors (linear and two-dimensional). The sensor is rotated by known angles under illumination from a stationary Xe arc-lamp light source on a two-axis rotary stage.

1 7

Type	Sun-sensor calibration bench —
Rotary stage	±100° vertical axis; unlimited horizontal axis —
Angle-setting accuracy	0.002 °
Light source	Xe arc lamp (Newport 6258), 5800 K —
Illuminance at sensor plane	30,000–140,000 lx
Irradiance at sensor plane	1000–3900 W/m²
Total angle-setting error	≤ 0.1 °

Modular CubeSat / SmallSat bus 6U–50 kg used as core platform for EO and tech-demo missions.

2 11

Bus class	TabletSat —
Form factor	6U–12U / SmallSat —
Wet mass	6–50 kg
Payload mass	up to 25 kg
Payload power	up to 50 W (orbit-avg)
Data downlink	up to 100 Mbit/s X-band
TT&C	UHF + S-band —
ADCS	3-axis stabilized —
Pointing	< 0.5 deg (3σ)
Design life	3–5 years
Target orbits	LEO, SSO —

"Vyunok" is an educational ground complex for receiving spacecraft radio signals, designed for experiments by schoolchildren and students. It operates within amateur-radio VHF/UHF regulations and suits contests and educational programs.

1 9

Type	Educational SDR receiving station —
Frequency range	136–146 MHz, 435–438 MHz —
Max data rate	≥ 9600 bit/s
Polarization	RHCP (right-hand circular) —
Antenna gain at zenith	3–4 dBi
LNA noise figure	≤ 1.6 dB (435–438 MHz) —
Protocols	APT, LRPT, AX.25, USP (GMSK), SSTV —
Modulations	FSK/GFSK/GMSK, BPSK, QPSK, FM, AM, SSB —
Receive chain	SDR —

Satellite reception and control ground station for mission control centers and education. Receives telemetry from small spacecraft in LEO and uplinks commands. The "Zavitok-M" (SXL-GND-02-M) works in VHF/UHF; the "Zavitok-S/L" (SXL-GND-02-SL) adds an S- and L-band parabolic antenna for payload-data reception.

1 12

Type	SDR satellite ground station —
Survey antennas	2 × quadrifilar (VHF/UHF receive) —
Directional antennas	2 × helical stack (UHF RX/TX) —
RX frequencies	136–146 MHz, 430–440 MHz —
TX frequencies	430–440 MHz (400–402 MHz) —
TX output power	10 W (40 dBm) —
Polarization	Circular RHCP —
LNA noise figure	≤ 1.6 dB (435–438 MHz) —
Protocols	APT, LRPT, AX.25, USP (GMSK), SSTV —
Modulations	FSK/GFSK/GMSK, BPSK, QPSK, FM, AM, SSB —
S/L variant adds	1.6 m parabolic, S 2230–2290 / L 1690–1710 MHz, up to 4 Mbit/s —
Variants	SXL-GND-02-M (VHF/UHF), SXL-GND-02-SL (+S/L band) —

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Sputnix

About Sputnix

Photos 5

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CubeSat Payload Development Tools

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Mission Control Center (MCC)

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OrbiCraft-Pro 1U CubeSat Platform

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OrbiCraft-Pro 3U CubeSat Platform

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OrbiCraft-Pro Educational CubeSat Kit

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Pallada Microsatellite Platform

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SG3 CubeSat Platform (4U / 16U)

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SX-GND-03 Laboratory UHF Transceiver

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SX-SBOX ADCS Actuators (Microsatellite)

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SX-SBOX ADCS Sensors (Microsatellite)

SX-SBOX ADCS Sensors (Microsatellite)

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SX-SBOX Communications (Microsatellite)

SX-SBOX Communications (Microsatellite)

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SX-SBOX Onboard Computing (Microsatellite)

SX-SBOX Onboard Computing (Microsatellite)

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SX-SBOX Power System (Microsatellite)

SX-SBOX Power System (Microsatellite)

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SX-SBOX Thermal Control (Microsatellite)

SX-SBOX Thermal Control (Microsatellite)

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SXC-FW4-02 Reaction Wheel Assembly

SXC-FW4-02 Reaction Wheel Assembly

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SXC-MB-04-ADC Onboard Computer with ADCS

SXC-MB-04-ADC Onboard Computer with ADCS

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SXC-PSS-03 Electrical Power System (with Battery Pack)

SXC-PSS-03 Electrical Power System (with Battery Pack)

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SXC-SD-01 Sun Sensor

SXC-SD-01 Sun Sensor

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