220N Monopropellant Thruster
Exact Nammo Space 220N hydrogen peroxide monopropellant RACS thruster model under development for attitude control. Nammo specifies 87.5% hydrogen peroxide propellant, 220 N nominal vacuum-class thrust, 160 s steady-state specific impulse, and more than 200,000 N·s total impulse; first application is planned for the Vega-C upper stage. Lifecycle remains development, and no vehicle-family installation is asserted here.
Identity
- Aliases
- 220N Hydrogen Peroxide Monopropellant Thruster220N H2O2 Thruster
- Domains
- spaceflight
- Identity Level
- model
- Kind
- chemical-thruster
- Name
- 220N Monopropellant Thruster
- Status
- development
Details
- Description
- Exact Nammo Space 220N hydrogen peroxide monopropellant RACS thruster model under development for attitude control. Nammo specifies 87.5% hydrogen peroxide propellant, 220 N nominal vacuum-class thrust, 160 s steady-state specific impulse, and more than 200,000 N·s total impulse; first application is planned for the Vega-C upper stage. Lifecycle remains development, and no vehicle-family installation is asserted here.
- Developers
- Manufacturers
- Propellants
- 87.5% hydrogen peroxide
- Rocket Specs
- Vacuum Specific Impulse
- …
- Vacuum Thrust
- …
Links
Assets & Meta
- Creation Time
- August 15, 2026 at 04:36:50 UTC
- Updated Time
- August 21, 2026 at 14:13:54 UTC
Other
- Sources
- Accessed Date
- 2026-08-21
- Note
- Nammo specifies the 220N RACS thruster as a hydrogen peroxide monopropellant unit using 87.5% hydrogen peroxide, with 220 N nominal vacuum-class thrust, 160 s steady-state specific impulse, more than 200,000 N·s total impulse, and a first application planned for the Vega-C upper stage.
- Publisher
- Nammo
- Title
- 220N Monopropellant Thruster