420N HTP Bipropellant Kick-Stage Engine
Thaliana Space420 N-class bipropellant rocket engine using 98% hydrogen peroxide as oxidizer, developed under ESA's GRACE 1/2 programs and…
123 satellite platforms, components and ground equipment from manufacturers worldwide.
420 N-class bipropellant rocket engine using 98% hydrogen peroxide as oxidizer, developed under ESA's GRACE 1/2 programs and…
Blowdown monopropellant propulsion system using 98% HTP with four 1 N thrusters for LEO small-satellite orbital maneuvers, attitude…
MEMS-manufactured propulsion system combining water electrolysis and hydrogen-oxygen catalytic combustion in a chip-based thruster, scalable from CubeSats to…
The MT-B is a bipropellant liquid rocket engine with a single regeneratively cooled thrust chamber, designed for the…
The MT-B is a bipropellant liquid rocket engine with a single regeneratively cooled thrust chamber, designed for the…
The AIS-SWAG1-QUAD is a Sublimation Warm Gas Thruster designed for CubeSats, offering 480uN of thrust and a total…
Staged-combustion LH2/LOX core stage engine for NASA's Space Launch System, evolved from the Space Shuttle Main Engine.
Bradford ECAPS (part of Bradford Space) is a Swedish space propulsion company developing High Performance Green Propellant (HPGP)…
Bradford ECAPS (a subsidiary of Bradford Space) is a Swedish aerospace company and world leader in High Performance…
A bipropellant thruster designed for the Briz-M booster, providing attitude control for spacecraft using UDMH/NTO propellants.
The RD-171 M is a powerful liquid rocket engine designed for the first stage of the Zenit launch…
The RD-180 is a liquid rocket engine with afterburning of oxidizing gas, designed for the first stage of…
The RD-181 is a liquid rocket engine with afterburning of oxidizing gas, designed for the first stage of…
RD-120MS is a modification of the RD-120 liquid rocket engine with afterburning of oxidizing gas, intended for the…
A hydrazine thermocatalytic low-thrust engine used for spacecraft orientation, attitude control, and station keeping.
Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…
The TU1 Thruster Unit is a thermocatalytic low thruster designed for spacecraft orientation and attitude control, using hydrazine…
The TU3 Truster Unit is a propulsion system designed for spacecraft orientation and attitude control, utilizing three modified…
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