ADCS & Navigation — Space Hardware Marketplace

Pulsar Verified Receiver Integration Program

• Signal compatibilityX1 (adj. GPS L1) and X5 (adj. GPS L5) L-band signals
• Integration methodFirmware/software update to existing dual-band GNSS receivers
• Inaugural verified partnersTrimble, Septentrio (Hexagon), STMicroelectronics, Safran, StarNav, Keysight

Xona's hardware certification ecosystem enabling GNSS receiver OEMs and chipset integrators to validate and ship Pulsar-compatible devices via…

CCD47-10 – Low-Noise Back-Illuminated CCD for Fine Guidance and Star Trackers

• Format1024 × 1024 pixels
• Pixel size13 × 13 µm
• ArchitectureBack-illuminated

1024×1024 back-illuminated CCD with very low readout noise for fine guidance sensors, star trackers, and precision wavefront sensing…

N-SPHERE – High-End GNSS Receiver

• SubsystemACDS Subsystem
• Component typeGNSS/GPS Receiver
• Form factorSmallSat

N-SPHERE is Syrlinks' high-end GNSS receiver for Real-Time Precise Onboard Orbit Determination (P2OD) and accurate time synchronization on…

AI-Q-2020 Navigation Grade Quartz Accelerometer (±60g, 220 µg)

Navigation-grade quartz accelerometer, ±60g, <220 µg bias repeatability, with temperature compensation.

AI-Q-2030 Navigation Grade Quartz Accelerometer (±60g, 160 µg)

Navigation-grade quartz accelerometer, ±60g, <160 µg bias repeatability, internal temperature model.

AI-Q-550 Control Grade Quartz Servo Accelerometer (±80g)

Miniature control-grade quartz accelerometer, ±80g, <1000 µg bias repeatability, 250g shock, 25.8g.

ARIETIS-NS 3-Axis Rad-Tolerant Space Gyroscope System

Space-qualified 3-axis CVG for LEO/GEO/MEO, 30krad TID, ITAR-free, serial production, 16-year lifetime.

GI-CVG-U-Series 1 & 2-Axis Gyroscope

1 or 2-axis tactical CVG, <10°/hr full-temp bias stability, <0.22°/hr in-run, RS-422 or analog output.

GI-CVG-N-Series 1 & 2-Axis Gyroscope (Tactical/Industrial Grade)

1 or 2-axis CVG with <10°/hr full-temp bias stability, <0.22°/hr in-run, 500K+ hr MTBF.

GI-CVG-A23XXD A-Series 3-Axis CVG Digital Gyroscope

3-axis Coriolis Vibratory Gyroscope with RS422 digital output, 0.3°/hr bias stability, 500K+ hr MTBF.

Ranging and Nanosatellite Guidance Experiment (RANGE)

• Project sponsorTerra Bella (formerly Skybox) University Cubesat Partnership
• Start date08/25/2015
• Faculty investigatorDr. Brian Gunter

RANGE is a mission consisting of two 1.5U CubeSats designed to demonstrate improved absolute orbital position knowledge and…

Star Sensor

• TypeStar tracker / star sensor for attitude determination
• DeveloperLSOT, XIOPM, Chinese Academy of Sciences

Star sensor technology for spacecraft attitude determination by XIOPM LSOT.

Micro VPS

The Theseus Micro VPS (Visual Positioning System) is a plug-and-play GPS-denied navigation module for Group 1 drones and…

Flywheel Aerospace Momentum Storage Systems

• TechnologyFlywheel momentum/energy storage
• ApplicationSatellite attitude control
• CountryIndia

Indian company developing flywheel-based momentum and energy storage systems for satellite attitude control applications.

BDStar Navigation Receivers

• ProductsBeiDou GNSS receivers, chips, terminals
• Systems supportedBeiDou (BDS), GPS, GLONASS, Galileo

Chinese BeiDou navigation satellite system receiver manufacturer, producing GNSS chips and receivers for satellite and terrestrial applications.

N-SPHERE Space GNSS Receiver

• Position accuracy< 0.5 m (P2OD algorithm)
• ConstellationsGPS, GALILEO, BeiDou, GLONASS
• Radiation tolerance15 krad TID

Software-Defined Radio GNSS receiver with sub-0.5m position accuracy and Real-Time Precise Onboard Orbit Determination, selected for LeoStella LS-300…

STIM210 MEMS Gyroscope Module

Compact tactical-grade MEMS gyroscope module with 0.3 deg/hr bias stability, LEO-proven on over 30 satellite programs since 2012.

SiREUS Inertial Reference Unit

• TechnologyHemispherical Resonator Gyroscope (HRG)
• Moving partsNone (solid-state)
• ApplicationSatellite AOCS inertial navigation

Space-grade hemispherical resonator gyroscope (HRG) inertial reference unit for satellite navigation and attitude control.