GP-LAM Liquid Apogee Module
Manastu Space300N modular green propulsion Liquid Apogee Module for launch vehicle upper stages, OTVs, and GEO spacecraft — multi-restart…
123 satellite platforms, components and ground equipment from manufacturers worldwide.
300N modular green propulsion Liquid Apogee Module for launch vehicle upper stages, OTVs, and GEO spacecraft — multi-restart…
Next-generation water-electrolysis propulsion system integrating low- and high-thrust maneuver capability in one unit — for satellites, interplanetary drones,…
Compact water-electrolysis propulsion system for nanosatellites and small satellites — 1.4 kg, >2.5 N thrust, >300s Isp, 5…
Monolithic metallic additively manufactured liquid oxygen / methane reaction control system (RCS) thruster.
Custom hybrid solid-liquid propulsion system solutions for CubeSats through ESPA Grande-class satellites, designed and integrated in-house.
High-performance hydrogen peroxide / HTPB fueled hybrid rocket upper stage for small launch vehicles.
Dawn Aerospace offers a family of non-toxic 'green' chemical propulsion thrusters (B1, B5, B20, B200) using nitrous oxide…
Northrop Grumman offers a comprehensive range of propulsion products and services, including flight-proven systems, bipropellant and monopropellant thrusters,…
High-endurance HPGP monopropellant thruster delivering 5.5-22 N thrust for AOCS and delta-V maneuvers on medium satellites.
High-thrust HPGP monopropellant engine delivering 50-200 N for reaction control system (RCS) applications.
Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.
Green propellant thruster variant delivering 1 N thrust for low-toxicity attitude control and delta-V maneuvers.
Low-toxicity ADN-based HPGP monopropellant thruster delivering 0.1 N thrust for AOCS and small delta-V maneuvers.
Flight-proven HPGP monopropellant thruster delivering 0.25-1 N thrust, used for AOCS and delta-V on CubeSats to smallsats.
Mid-class HPGP monopropellant thruster delivering 1.4-5.5 N thrust for AOCS and delta-V on small and medium satellites.
Space-qualified pressure transducer, 1–310 bar range, ±0.3% FS BoL accuracy, 250 g, compatible with hydrazine, MON, MMH and…
Ultra-compact 180 g space-qualified pressure transducer, 3–320 bar range, ±0.3% FS accuracy, for small spacecraft propulsion systems.
Dawn Aerospace offers a range of non-toxic 'green' chemical propulsion thrusters (B1, B5, B20, B200) using nitrous oxide…
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