220N Monopropellant Thruster
Nammo’s 220N hydrogen-peroxide monopropellant RACS thruster uses 87.5% H2O2. The manufacturer lists nominal thrust of 220 N and a separate nominal sea-level value of 148 N. Vacuum specific impulse is 160 s in steady-state firing and 130 s in pulse firing; the structured 160 s rating represents steady-state operation. Nammo describes development and qualification for a planned Vega-C AVUM+ application.
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
- Nammo’s 220N hydrogen-peroxide monopropellant RACS thruster uses 87.5% H2O2. The manufacturer lists nominal thrust of 220 N and a separate nominal sea-level value of 148 N. Vacuum specific impulse is 160 s in steady-state firing and 130 s in pulse firing; the structured 160 s rating represents steady-state operation. Nammo describes development and qualification for a planned Vega-C AVUM+ application.
- Developers
- Manufacturers
- Propellants
- 87.5% hydrogen peroxide
- Rocket Specs
- Sea Level Thrust
- …
- Vacuum Specific Impulse
- …
- Vacuum Thrust
- …
Links
Assets & Meta
- Creation Time
- August 15, 2026 at 04:36:50 UTC
- Updated Time
- October 17, 2026 at 00:53:16 UTC
Other
- Sources
- Accessed Date
- 2026-10-17
- Note
- Manufacturer lists nominal 220 N thrust, nominal 148 N at sea level, and vacuum specific impulse of 160 s in steady-state firing versus 130 s in pulse firing. Development and qualification remain the product-page status.
- Publisher
- Nammo
- Title
- 220N Monopropellant Thruster