Space Hardware Marketplace

Ninox eSWIR 640 Space Camera

• Spectral rangeExtended SWIR (eSWIR), beyond 2 µm
• Format640 pixels
• ApplicationsHyperspectral imaging, night-time surveillance, thermal and mineral remote sensing

Extended-SWIR 640-pixel space camera for hyperspectral, thermal, and night-time remote sensing payloads on LEO CubeSats.

Eagle 47-10 Space Camera

• SensorBack-illuminated 1MP CCD (Teledyne e2v)
• Pixel size13 µm x 13 µm
• Peak QE>90% @ 525 nm; 50% @ 380 nm and 720 nm

Deep-cooled back-illuminated 1MP CCD space camera with 7-year vacuum guarantee and >90% QE at 525 nm for LEO…

RapidCube-20 CubeSat Bus

• CubeSat class20 kg
• Size (stowed)22 x 22 x 44 cm (16U)
• Bus architectureFailure-tolerant

16U, 20 kg CubeSat bus with failure-tolerant architecture supporting 5–10 kg payloads, S/X-band links, and SSO IOD/IOV missions.

RapidCube-6 CubeSat Bus

• CubeSat class8 kg
• Size (stowed)22 x 10 x 36 cm (6U) / 22 x 10 x 45 cm (6U XL)
• Bus architectureFailure-tolerant

6U CubeSat bus platform with failure-tolerant architecture, S/X-band links, and configurable attitude control for LEO missions up to…

RK410 High Reliability Space OCXO

• Package size (LxWxH)99 x 88 x 54 mm
• Nominal frequency5 to 10 MHz
• Stability class10^-10

MIL/ECSS-qualified space oscillator with 10^-10 stability class, used operationally by international space agencies for decades.

SpectraLoc Payload

• CapabilitiesPassive emitter detection, classification, direction-finding, geolocation
• Detection rangeExtended line-of-sight
• Platform compatibilityFixed-wing drones, quadcopters, VTOL platforms (small UAVs)

Compact airborne RF payload for passive threat detection, direction-finding, and geolocation, built for small UAV integration.

Quadsat Antenna Measurement System

• Measurement capabilitiesPointing accuracy, tracking and handover, radiation pattern raster and cut, cross-polar discrimination, gain, EIRP, G/T
• Antenna types supportedMulti-beam, flat-panel, electronically steerable (LEO and multi-orbit)
• Lifecycle coverageManufacturing QC, vendor type approval, factory/site acceptance testing, in-situ deployment calibration, ongoing performance monitoring

Drone-based satellite antenna test and calibration system supporting the full antenna lifecycle, tailored for LEO and multi-orbit terminals.

ADCS control unit

• Dimensions, mm101 x 100 x 20 (without fasteners)
• Mass, g220
• Power voltage, V6-36 (without galvanic isolation)

A dual-redundant attitude control and stabilization system control unit (OSSCU, SX-SBOX-ADCU-01) running SPUTNIX's flight-qualified ADCS software.

Reaction wheel

• Dimensions, mm160 x 160 x 80 (without fasteners)
• Mass, kg3.2
• Power voltage, V22-34 (without galvanic isolation)

A control flywheel motor (CFM, SX-SBOX-RWH-50-2.0-01) generating control torque via rotor acceleration/deceleration for larger satellite platforms.

Magnetic torquers

• Model SX-MT-1Maximum moment 1 A*m2, Consumption 0.4 Wt, Mass 200 g, Diameter 16 mm, Dimensions 140x30x30 mm
• Model SX-MT-5Maximum moment 5 A*m2, Consumption 0.6 Wt, Mass 350 g, Diameter 20 mm, Dimensions 220x50x35 mm
• Model SX-MT-10Maximum moment 10 A*m2, Consumption 0.7 Wt, Mass 550 g, Diameter 20 mm, Dimensions 320x50x35 mm

A family of proprietary magnetic torquer rods (SX-MT-1 through SX-MT-30) used with the magnetic torquers control unit for…

Magnetic torquers control unit

• Dimensions, mm54 x 48 x 20 (without fasteners)
• Mass, g85
• Power voltage, V6-36 without galvanic isolation

A control unit (SX-SBOX-MTQU-01) driving up to three magnetic torquers via PDM channels to implement angular velocity damping…

Magnetometer

• Dimensions, mm54 x 52 x 16 (without fasteners)
• Mass, g70
• Power voltage, V6-36 without galvanic isolation

A triaxial anisotropic-magnetoresistive magnetometer (SX-SBOX-MAG-01) used in attitude determination alongside magnetic torquers for detumbling and momentum unloading.

Solar sensor

• Dimensions, mm43 x 43 x 16 (without fasteners)
• Mass, g45
• Power voltage, V6-36 without galvanic isolation

A compact sun sensor (SX-SBOX-SUNS-01) for the attitude control loop, with algorithms mitigating Earth-albedo glare, suitable for microsatellites…

Fibre-Optic Gyroscope

• Dimensions of the sensor unit275 x 275 x 160 mm (without fasteners)
• Dimensions of the control unit171 x 111 x 44 mm (without fasteners)
• Power voltage, V22-34, galvanic isolation 500V

A high-precision fibre-optic gyroscope (FOG, SX-SBOX-AVS-FOG-01) with a control unit and 4-element sensitive assembly (3 main + 1…

Satellite navigation equipment

• Dimensions, mm171 x 111 x 51 (without fasteners)
• Mass, kg0.7
• Power voltage, V22-34, galvanic isolation 500V

A GNSS receiver unit (SX-SBOX-GNSS-01) providing precision position, velocity and time synchronization for the spacecraft.

Angular velocity sensor

• Dimensions, mm54 x 52 x 20 (without fasteners)
• Mass, g75
• Power voltage, V6-36 without galvanic isolation

A triaxial MEMS-based angular velocity sensor (SX-SBOX-AVS-MEMS-01) for small satellite attitude determination.

Reaction wheels module

A 4-flywheel reaction wheel module (SXC-FW4-02) for CubeSat 3-axis attitude control, integrating drivers and control electronics on a…

Control unit of the thermal regime support system

A redundant thermal control unit (SX-SBOX-THERMU-01) that monitors and manages heaters based on analog/digital temperature sensors across the…