Payloads & Instruments — Space Hardware Marketplace

ERB-2 — Erasmus Recording Binocular 2

• FunctionDigital stereoscopic (binocular) camera
• TSD scopeFlight electronics and ground segment
• LaunchFebruary 2010, ISS

Digital stereoscopic camera for the ISS simulating human binocular vision, with TSD flight electronics and ground segment.

Camera System for Small Space Platform (PRISMA H2VMU)

• Resolution4 Mpixel
• FunctionsReal-time color video acquisition, compression, storage, encoding
• MissionPRISMA (Mango/Tango), launched 15 June 2010, operated until August 2014

Real-time color video acquisition, compression and encoding unit flown on the PRISMA formation-flying mission.

DVS for ISS Scientific Payloads

• Resolution / frame rateup to 4 Mpixels @60 fps
• High frame rate mode~1000 fps @512x512 px
• CompressionWavelet-based

Digital video system for the ISS EML facility supporting high frame rate and high resolution video acquisition.

MOSS — Multi-Ocular Smart Systems

• Camera configuration1 trinocular camera + 2 monocular cameras
• Video inputsUp to 4 HD video inputs
• Video data throughput240 Mpixel/s

Vision-based navigation camera suite with trinocular/monocular cameras and a high-performance processing unit.

Compact Camera for Small Earth Observation Satellites (STREEGO)

12Mpixel Earth observation camera payload developed for ESA's STREEGO small-satellite program.

H2CS-1 — Highly Compact Camera System for CubeSat

Dual-FOV CubeSat camera system with motorized autofocus primary lens and wide-field secondary imager.

H2CS-2 — Highly Compact Camera System for CubeSat

Compact 4Mpixel CubeSat camera with SpaceWire and Camera Link interfaces, thermo-mechanically decoupled focal plane.

H2CS-3 — Highly Compact Camera System for CubeSat

• Design goalCompact, low mass, low power, fully autonomous
• ProcessingEmbedded on-board imaging algorithms

Compact, low-power, low-mass CubeSat camera system, fully autonomous with embedded image processing.

SMC — Spacecraft Monitoring Camera

Very compact deep-space CMOS monitoring camera developed for ESA's HERA mission.

Umbra Scan Wide-Area SAR Imagery

• Sensor TypeSynthetic Aperture Radar (SAR)
• Resolution Range50 cm to 2 m
• FootprintUp to 8 km x 100 km

Cross-track, wide-area SAR imagery with resolutions from 50 cm to 2 m and footprints up to 8 km…

Umbra Dwell SAR Imagery

• Sensor TypeSynthetic Aperture Radar (SAR)
• Product TypesEnhanced-detail GeoTIFF, Color Sub-Aperture Image (CSI), SAR video
• Max SAR Video Length25 seconds

Extended-collection SAR product using Umbra's agile squint capability to reduce speckle and detect/classify moving objects, including SAR video…

Umbra Spotlight SAR Imagery

• Sensor TypeSynthetic Aperture Radar (SAR)
• Best Resolution25 cm (ground-projected)
• Resolution Options25 cm, 35 cm, 0.5 m, 1.0 m

Record-breaking-resolution commercial SAR imagery, delivering true 25 cm ground-projected resolution with up to 1200 MHz bandwidth.

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.