30kN Hybrid Engine
Nammo
The 30kN Hybrid Engine is a rocket engine developed by Nammo Raufoss AS, designed for space propulsion applications.
Typed specifications17 values
Discloses 8 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- hybrid datasheet p.1
- Mass
- 165 kg engine mass including fuel cartridge · datasheet p.1 165 kg including fuel cartridge
- Thrust
- 30 000 000 mN in vacuum · datasheet p.2
- Envelope (L×W×H)
- 356mm [14 inch] Diameter, 1.7m Length datasheet p.2
- Specific impulse
- 270 s datasheet p.2
- Total impulse
- 1 000 000 N·s min · datasheet p.2 1 000 000 N·s min · >1000 kNs
- Propellant
- 87.5% H2O2, and HTPB datasheet p.2 HTP (hydrogen peroxide) 87.5% H2O2 | HTPB
- TRL
- 8 datasheet p.1
- Thruster technology
- hybrid motor datasheet p.1
- Max continuous burn
- 40 s thrust duration · datasheet p.1
- Flight heritage
- TRL8, flown on Nucleus Sounding Rocket datasheet p.2
- Ignition or start
- other no igniter or pyrotechnic components required · datasheet p.1
- Restartable
- yes Restarts: Possible · datasheet p.1
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier10 lines, in the manufacturer's own wording
- Thrust
- 30,000 N in vacuum
- Thrust Duration
- 40 seconds
- Engine Mass
- 165 kg
- Propellant Combination
- 87.5% H2O2, and HTPB
- Specific Impulse
- 270 seconds, in vacuum
- Total Impulse
- >1000 kNs
- Dimensions
- 356 mm Diameter, 1.7 m Length
- Materials
- Stainless Steel construction
- Fluidic Interface
- 2 inch Tubing for Oxidiser feed
- Technology Readiness Level
- TRL8
About
The 30kN Hybrid Engine is a propulsion system developed by Nammo Raufoss AS. While specific details regarding its purpose, how it works, features, configurations, and flight heritage are not provided on this product page, its classification as a ‘Hybrid Engine’ and its placement within the ‘Space Propulsion Thrusters and Engines’ category on the manufacturer’s website indicate its intended use in space applications. The engine is capable of producing 30 kilonewtons of thrust.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.