Chemical Propulsion — Space Hardware Marketplace

Propulsion market benchmark: medians, lead times & prices →

40 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.

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Chemical Propulsion

D-Start Micro-Propulsion Engine

d-start
  • TypeMicro-propulsion engine
  • Target platformCubeSat, microsatellite

Russian small satellite propulsion engine developed under the 2035 University project, providing thrust for CubeSat and microsatellite maneuvering.

Chemical Propulsion

HIP_11 Propulsion System

ISPTech
  • PropellantH2O2 (hydrogen peroxide) + ionic liquid fuel
  • Specific impulse (vacuum)Up to 310 s
  • Propellant storage density (H2O2)Up to 1,440 kg/m3

Advanced green hypergolic H2O2 + ionic liquid multi-mode propulsion, up to 310 s Isp, 20-200 N.

Chemical Propulsion

HyNOx-200 Thruster

ISPTech
  • Thrust range (demonstration target)100-400 N
  • Specific impulse (vacuum target)Up to 285 s
  • Continuous operation (vacuum target)>15 minutes

Large-scale 100-400 N green bipropellant thruster, up to 285 s Isp, available Q2 2026.

Chemical Propulsion

HyNOx-22 Thruster

ISPTech
  • Thrust range11-44 N
  • Specific impulseUp to 280 s
  • Continuous operation>15 minutes

11-44 N green bipropellant thruster with vacuum heritage, >4,000 ignitions, up to 280 s Isp.

Chemical Propulsion

HyNOx-5 Thruster

ISPTech
  • Thrust range (target)2.5-10 N
  • Specific impulse (vacuum target)Up to 280 s
  • Continuous operation (vacuum target)>10 minutes

Mid-range 2.5-10 N green bipropellant thruster using N2O/ethane, up to 280 s Isp, available Q4 2026.

Chemical Propulsion

HyNOx-1 Thruster

ISPTech
  • Thrust range0.5-2 N
  • Specific impulse (hot gas)Up to 270 s
  • Continuous operation16 minutes

0.5-2 N green bipropellant thruster using N2O/ethane, up to 270 s Isp, >13,000 ignitions demonstrated.

Chemical Propulsion

CHIPS CubeSat High Impulse Propulsion System

CU Aerospace
  • Propellant optionsR236fa and R134a (range-safety approved)
  • CHIPS-180 size0.54U
  • CHIPS-180 total impulse180 N-s

Miniaturized propulsion combining main thruster with 3-axis attitude control — non-toxic self-pressurizing propellants, 120M+ valve actuations, 0.54U CHIPS-180…

Chemical Propulsion

CubeHood Propulsion Module

DREAM Aerospace
  • Compatible platforms1U to 26U+ CubeSats
  • AssemblyReady-to-use, no additional assembly required

All-in-one, ready-to-use propulsion module integrating with the ATOM thruster — combines fuel tanks and thrust control for CubeSat…

Chemical Propulsion

ATOM Monopropellant Thruster

DREAM Aerospace
  • ThrustStarting from 1N
  • Compatible platforms1U to 26U+ CubeSats
  • PropellantEco-friendly, nontoxic monopropellant

Next-generation monopropellant thruster using eco-friendly, nontoxic propellant — starting from 1N thrust, for 1U to 26U+ CubeSats, 30x…

Chemical Propulsion

GATE Thruster

GATE Space
  • Thrust (S/M/L)2-20N / 5-50N / 20-200N
  • Throttling ratio1:10
  • Min impulse bit0.2Ns / 0.5Ns / 2Ns

High-performance thruster with closed-loop pressure control and deep throttling — 2-200N thrust range across 3 sizes, up to…

Chemical Propulsion

GATE Jetpack Propulsion Module

GATE Space
  • Total impulse (S/M/L)36,000 / 80,000 / 140,000 Ns
  • Thrust (S)4x [1-6N]
  • Thrust (M/L)4x [20N]

Plug-and-play chemical propulsion module for ESPA-class satellites — 3 sizes (S/M/L), 36,000-140,000 Ns total impulse, orbit transfer and…

Chemical Propulsion

DARUMA Micro Hybrid Propulsion Unit

Letara
  • Wet mass30 kg
  • Performance (10kg payload)Accelerates to 1,100 m/s
  • Performance (100kg payload)Accelerates to 400 m/s

Modular hybrid propulsion unit using solid HDPE fuel and N2O oxidizer for last-mile orbital maneuvers of small satellites…

Chemical Propulsion

BOOSTER Green Propulsion System

Liftero
  • Thrust classes1N (0.49-1.42N), 5N (2.62-7.62N), 20N (10.5-30.5N), 200N (138-241N)
  • Specific impulse273-303 s (varies by class)
  • PropellantsN2O + C2H6

Modular green chemical propulsion system family for small satellites — thrust classes from 1N to 200N, N2O/C2H6 propellants,…