ProductUpdated on 4 November 2025
ISPTech HyNOx Thrusters
Founders Associate at ISPTech - InSpacePropulsion Technologies
Hardthausen, Germany
About
Status
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Demonstrator under testing
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Customer projects ongoing, IOD 2026
Thruster classes
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HyNox-200 Thruster (50-400 N)
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HyNOx-22 Thruster (11-44 N)
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HyNOx-5 Thruster (2.5-10 N)
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HyNOx-1 Thruster (0.5-2.0 N)
Your benefits
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Green, affordable and easily available propellants: N2O + C2H6
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Simple system architecture – self-pressurized system
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Thrust level can be controlled by propellant temperature control
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Thermal steady-state operation of the thruster allows significant deltaV from a single maneuve
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ITAR free and REACH compliant
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Cold-start capable
Capabilities
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Propellant feeding: Liquid or gaseous, depending on mission requirements
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Thruster operatable for saturated fluid temperatures, typically -29°C to +32°C, extensions are possible, and the system survivability temperature range can be customizable (up to 71°C qualified)
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Services offered: CAD Design and Feeding System Layout, Modelling of thrust, propellant consumption, tank and feeding system conditions, Propulsion system integration and experimental characterization, Thruster acceptance testing, On-site AIT support, Fueling
Looking for
- Buyer
- Demonstration / Pilot projects
Applies to
- Earth observation
- Engines
- Equipment
- Satellite navigation
- Space
- Space exploration
- Space technology
Attached files
Organisation
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