123 satellite platforms, components and ground equipment from manufacturers worldwide.
445 N (100 lbf) high performance bipropellant apogee engine, available in dual mode configuration; the R-4D lineage is…
The Apogee Engine Valve is a single-stage, redundant solenoid coil thruster flow control device specifically designed for propulsion…
Liquid hydrogen / liquid oxygen upper-stage engine family powering Atlas V, Delta IV Heavy, Vulcan Centaur and NASA…
The Green Monopropellant Propulsion System developed by Yuzhnoye SDO is intended for generating thrust impulse bits to extend…
Launcher's E-2 liquid oxygen/RP-1 rocket engine — a 22,000 lbf thrust engine developed using advanced manufacturing for Launcher…
CNNC Space's research into nuclear thermal propulsion (NTP) systems and radioisotope thermoelectric generators for China's deep-space exploration program.
Astro Mechanica's electric jet engine augmented rocket first stage — using turbine-driven air-breathing propulsion at low altitude to…
Promin Aerospace's Prometheus-1 — a Ukrainian-developed liquid propellant rocket engine for small orbital launch vehicles and sounding rockets.
MT Aerospace's lightweight composite overwrapped pressure vessels (COPVs) and cryogenic propellant tanks for launch vehicles and satellites —…
High-thrust LOX/LNG rocket engine powering New Glenn and Vulcan Centaur, designed for high reusability.
VACCO's Integrated Propulsion System (IPS) is a complete, bolt-on propulsion module for SmallSats, providing attitude control and delta-V…
AF-M315E (ASCENT) is a high-performance, less toxic green monopropellant developed by AFRL and licensed to DSSP, offering an…
HAN-based electrically-ignited monopropellant, comparable to AF-M315E with faster ignition.
The PEPT-420N is a large-volume spherical titanium propellant tank with 37.5 liters nominal volume and 30 kg maximum…
The PEPT-260 is a spherical titanium propellant tank with 9.3 liters nominal volume for hydrazine monopropellant propulsion systems.…
The PEPT-230 (Positive Expulsion Propellant Tank) is a spherical titanium propellant tank with 6 liters nominal volume designed…
The Attitude Control Propulsion Unit (ACPU) developed by ISS Reshetnev provides thruster-based attitude control and fine station-keeping for…
The Rafael 200N Monopropellant Hydrazine Thruster is a high-thrust space propulsion unit designed for integration into Roll Attitude…
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