The HyNOx Technology
HyNOx utilizes nitrous oxide (N2O) and ethane (C2H6) as bipropellant. The benefits are:
- Non-toxic components and simple handling
- Low-cost, easily available substances
- Isp up to 300 s
- Self-pressurized propulsion systems
- Development on nitrous oxide based green propellants started in 2014, initially with focus on monopropellants
Our 22 N HyNOx thruster during hot firing in DLR's vacuum test facility
The HIP_11 Technology
HIP_11 is a novel patented hypergolic propellant based on hydrogen peroxide and an ionic liquid fuel.
HIP_11 features:
- Fast and reliable hypergolic ignition
- Significantly reduced toxicity compared to conventional hypergolic propellants
- Isp up to 310 s
- Developed at DLR Institute of Space Propulsion by Felix during his PhD project since 2017
- First successful demonstration of a hypergolic propellant based on an ionic liquid and hydrogen peroxide in a rocket thruster
Hypergolic ignition of HIP_11
© DLR Spin-off Project InSpacePropulsion Technologies. All rights reserved.
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