Space Hardware Marketplace

3P VibePOD

Open-source vibration test fixture for qualifying 3P PocketQube satellites.

2P VibePOD

Open-source vibration test fixture for qualifying 2P PocketQube satellites.

1.5P VibePOD

Vibration test fixture for qualifying 1.5P PocketQube satellites, flight-proven on AMSAT missions.

1P VibePOD

• Compatible satellite size1P PocketQube
• Qualification standardNASA GEVS7000 (random vibration)
• First flight qualificationFOSSASAT-1, Rocket Lab 'Running Out of Fingers' mission, Q4 2019

Vibration test fixture for qualifying 1P PocketQube satellites to NASA GEVS7000 standards.

Claymore 6P PocketQube Deployer

• CapacityUp to 6P PocketQube
• Compatible satellite sizes1P, 1.5P, 2P, 3P PocketQube
• Mechanical interfaceMeets PocketQube mechanical standard

Modular 6P PocketQube deployer with flight-proven release mechanisms for dispensing pico satellites.

XavSat-1 Mission Satellite

Ghana's first privately developed PocketQube satellite, flying a quantum temperature-and-pressure profiling payload.

XavSat PocketQube Satellite Bus (1P-3P)

• Form factorPocketQube, 1P-3P (5 cm cube unit)
• On-Board Computer (OBC)Atmega328P microcontroller
• Payload interfacesI2C, SPI, UART

Modular PocketQube nanosatellite bus in 1P-3P (5 cm form factor) configurations for rapid, low-cost orbital deployment.

XDSAT M400

Micro-satellite platform for 40-75 kg payloads supporting EO optical, SAR, SIGINT, IoT and laser missions.

XDSAT M600

Micro-satellite platform for payloads up to 300 kg, in-orbit qualified in 2026 with an India-built multispectral optical payload.

XDSAT M200

Micro-satellite platform for 25-40 kg payloads supporting EO optical, SAR, SIGINT, IoT and laser missions.

XDSAT NS

6U small satellite platform for EO optical, SAR, SIGINT, IoT and laser payloads with hosted-payload ISR mission support.

XDSAT NL

12U-16U small satellite platform for EO optical, SAR, SIGINT, IoT and laser payloads with 8U of payload volume.

CIS 300 Imager Control System

• SensorTeledyne e2v CIS 300
• FormatUp to 9k x 9k pixels
• Data Lines12

Imager control system for the Teledyne e2v CIS 300 sensor, supporting up to 9k x 9k pixel formats.

ChromaD Imager Control System

• SensorTeledyne e2v CHROMA-D (stitched SWIR detector for satellites)
• MonitoringBuilt-in temperature monitoring; voltage/current monitoring with automated shutdown
• Data InterfaceUSB 3

Imager control system for the Teledyne e2v CHROMA-D stitched SWIR satellite detector.

CIS 120 Imager Control System

• SensorTeledyne e2v 'Capella', 2k x 2k back-illuminated, 10 µm pixels
• ApplicationsVisible, UV, and EUV
• Noise3 e⁻ rms

Plug-and-play imager characterisation and control system for the Teledyne e2v Capella sensor.

CIS 125 Imager Control System

• SensorTeledyne e2v CIS 125 TDI
• FunctionalityTDI CCD functionality on a CMOS chip
• Data Lines20 lines for full format support

Imager control system for the Teledyne e2v CIS 125 TDI sensor with full-format Ethernet readout.

Space PFO

• ApplicationParticulate fallout monitoring inside launch vehicle fairings
• MeasurementFirst-of-kind measurements of particulate fallout during launch
• Monitoring ScopeEnclosed satellite payloads, mechanical/acoustic shock contamination

Space-based particulate fallout monitor measuring contamination inside launch vehicle fairings.

PFO 1040

• Monitoring TypeContinuous, real-time particle monitoring and analytics
• Particle Size Threshold> 5 µm
• DetectionContamination event and fallout trend detection

Ground-based real-time surface particulate fallout monitor for clean environments.