Payloads & Instruments — Space Hardware Marketplace

LPT 9310 HP COTS+ Pulse-Tube Cryocooler

5.7 W split pulse-tube cryocooler based on flexure-bearing technology, flown on NASA's ECOSTRESS instrument on the ISS.

LPT 9510 COTS+ Pulse-Tube Cryocooler

Compact split pulse-tube cryocooler delivering 1.4 W of cooling power at 80 K for IR detector cooling.

LPT6510 Pulse-tube Cryocooler

Designed-for-manufacturability pulse-tube cryocooler for 60 K and above, based on the flight-proven MPTC compressor.

ThumbSat

Femtosatellite-class hosted-payload module (~48x48x15-32mm, up to 25g) that flies student, research or artistic experiments to low Earth orbit…

FOVEA M2

• ConfigurationMonolithic Telescope + Stereo Camera Pair + Wide/Narrow FOV Center Camera
• Orbit ratingLEO Rated
• TypeHardware

LEO-rated multi-camera and telescope payload for resolved imagery.

FOVEA M1

• Video4K Full Motion Video
• Lens options8mm-60mm Lenses
• Dynamic rangeWide Dynamic Range

LEO-rated 4K full-motion video camera with interchangeable lenses.

TRICLOPS

• ConfigurationWide or Narrow FOV Camera + Stereo Camera Pair
• Orbit ratingGEO Rated
• TypeHardware

GEO-rated three-camera payload for rendezvous, proximity operations and docking.

QuadClops

• ConfigurationWide or Narrow FOV Center Camera + Stereo Camera Pair + 4th Camera
• Orbit ratingGEO Rated
• TypeHardware

GEO-rated multi-camera payload for stereo and wide-area situational awareness.

QuadClops Pro

• ConfigurationMonolithic Telescope + Stereo Camera Pair + Wide/Narrow FOV Center Camera
• Orbit ratingGEO Rated
• TypeHardware

GEO-rated multi-camera and telescope payload for resolved imagery and rendezvous operations.

GeoStare SV2 Electro-Optical Imaging Satellite

Electro-optical Earth observation smallsat using Lawrence Livermore National Laboratory sensor technology.

CDAS — Control & Data Acquisition Systems for Scientific Payloads

• ComponentsExperiment computers; real-time data processing subunits
• SensingTemperature, pressure, extensometers, accelerometers, strain gauges, force sensors
• ActuationStepper/DC/brushless motors, injection devices, heaters, peltiers

Experiment computers and data acquisition subsystems for scientific payloads and instruments.

Data Handling Unit for Foton Satellite Payload

• MissionsFOTON 12, M1, M2, M3
• FunctionsTC/TM and digital video handling
• Payload capacityUp to 10 experimental payloads (M3 mission)

Data handling unit managing telecommand, telemetry and digital video for up to 10 experimental payloads on Foton missions.

HYDRA — Hyperspectral Compression IP Core & HW Platform

• FPGARad-hard Xilinx Virtex XQR5XVFX130
• FamilyTSD 'HPxx' high-performance processing units
• Standards contributionBasis proposed for MHDC / CCSDS 123

FPGA-based hyperspectral compression IP core and hardware platform, contributing to the CCSDS 123 standard.

HSC-CB — High Speed Camera Compression Board for ISS EML Facility

• Form factorPC-104+ module
• Camera frame rate>30,000 fps
• Compression performance improvementFactor of 5

PC-104+ compression board improving compression chain performance for the ISS EML facility's high-speed camera.

Payload Data Processing Unit for Solar Orbiter SWA Instrument

• RedundancyFully redundant, rad-hard
• MissionESA Solar Orbiter
• Instrument suiteSWA (Solar Wind Analyzer): EAS1, EAS2, PAS, HIS

Fully redundant rad-hard data processing unit supporting the Solar Wind Analyzer instrument suite on ESA's Solar Orbiter.

SDAC — Multi/Hyperspectral High Data Rate Image Compression Module

• MissionPRISMA, operational since 22 March 2019, 615 km altitude
• Spectral range400–2500 nm (hyperspectral)
• RedundancyNominal + redundant boards

Scientific Data Acquisition and Compression module flown on the PRISMA hyperspectral Earth observation satellite.

Image Data Handling and Storage Unit for PILOT-D CDIU

• ProgramPILOT (Precise and Intelligent Landing using On-board Technologies)
• MissionLuna-25 / Luna-Glob lander
• FunctionsCommunications I/F, video storage/processing, power distribution

Image data handling, storage and power distribution unit for the PILOT-D camera demonstrator on the Luna-25 lander.

DVS for Sounding Rocket Experiment Modules

• Core unitH2VMU (High resolution/High frame rate Video Management Unit)
• ArchitectureModular, distributed
• Maiden flight2005, MASER 10 sounding rocket

Modular digital video system built around the H2VMU core unit, flown on multiple sounding rocket missions since 2005.