Space Hardware Marketplace

1 N GP Thruster

• Thrust0.25-1 N
• PropellantLMP-103S (ADN-based, non-toxic)
• FunctionAOCS + ΔV

Green propellant thruster variant delivering 1 N thrust for low-toxicity attitude control and delta-V maneuvers.

200 N HPGP RCS Thruster

• Thrust50-200 N
• Specific Impulse206-234 s
• Mass5.7 kg

Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.

200 N HPGP Thruster

• Thrust50-200 N
• Specific Impulse206-234 s
• Mass5.7 kg

High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.

22 N HPGP Thruster

• Thrust5.5-22 N
• Specific Impulse235-250 s
• Mass1.0 kg

High-endurance HPGP monopropellant thruster delivering 5.5-22 N thrust for AOCS and delta-V maneuvers on medium satellites.

5 N HPGP Thruster

• Thrust1.4-5.5 N
• Specific Impulse220-245 s
• Mass0.45 kg

Mid-class HPGP monopropellant thruster delivering 1.4-5.5 N thrust for AOCS and delta-V on small and medium satellites.

1 N HPGP Thruster

• Thrust0.25-1 N
• Specific Impulse204-231 s
• Mass0.39 kg

Flight-proven HPGP monopropellant thruster delivering 0.25-1 N thrust, used for AOCS and delta-V on CubeSats to smallsats.

100 mN HPGP Thruster

• Thrust0.1 N
• Specific Impulse≥190 s
• Mass0.04 kg

Low-toxicity ADN-based HPGP monopropellant thruster delivering 0.1 N thrust for AOCS and small delta-V maneuvers.

Acceleration Measurement Unit (AMU)

• ApplicationMicrogravity acceleration monitoring

Precision instrument for measuring microgravity acceleration levels aboard crewed and uncrewed spacecraft.

Cosine Sun Sensor Redundant (COSS-R)

• Angular ResponseCosine
• RedundancySelf-redundant

Self-redundant cosine-response sun sensor delivering reliable wide-angle solar position data for safe-mode operations.

Mini Fine Sun Sensor (Mini-FSS)

• Detector TypeAnalogue quadrant detector
• Axes2
• Form FactorCompact / lightweight

Compact, lightweight version of the Fine Sun Sensor for small satellites and CubeSats requiring precise sun-vector data.

Fine Sun Sensor (FSS)

• Detector TypeAnalogue quadrant detector
• Axes2
• Output4 quadrant voltages + sun presence voltage

Analogue quadrant-detector sun sensor providing precise two-axis solar aspect angle for yaw steering and earth-pointing missions.

Coarse Sun Sensor (CSS)

• Field of ViewHemispherical
• RedundancySelf-redundant
• In Production Since1975

Rugged self-redundant sun sensor delivering coarse solar position data for safe-mode and coarse maneuvering.

Bradford Standard Accuracy Pressure Transducer

• ModelStandard
• Max Pressure Range1–310 bar
• Accuracy (BoL)±0.3% FS

Space-qualified pressure transducer, 1–310 bar range, ±0.3% FS BoL accuracy, 250 g, compatible with hydrazine, MON, MMH and…

Bradford Miniaturised Pressure Transducer

• ModelMiniaturised
• Max Pressure Range3–320 bar
• Accuracy (BoL)±0.3% FS

Ultra-compact 180 g space-qualified pressure transducer, 3–320 bar range, ±0.3% FS accuracy, for small spacecraft propulsion systems.

Supernova High Power PCDU

High-power power conditioning and distribution unit for deep-space avionics and demanding satellite bus power architectures.

Bradford Redundant Cosine Sun Sensor (COSS-R)

• FOV160 × 160°
• Accuracy±3° (3σ) OBC-limited
• Resolution< 0.1°

Self-redundant cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 15 g ultralight, 0 W passive, >100 kRad TID.

Bradford Coarse Sun Sensor (CSS)

• FOV180 × 180°
• Accuracy±2° (3σ) at BoL
• Resolution< 0.1°

Internally-redundant coarse sun sensor with full-sky 180×180° FOV, ±2° accuracy, 215 g, dual 9-pin D-sub interface, >100 kRad…

Bradford Cosine Sun Sensor (CoSS)

• FOV160 × 160°
• Accuracy±3° (3σ) OBC-limited
• Resolution< 0.1°

Compact 25 g cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 0 W passive, >100 kRad TID, 30×30×14…