WEPA-Technologies GmbH
WEPA-Technologies GmbH

Liquid Propellant Rocket Engines

Engines using liquid propellants are preferred in applications requiring long operating time, re-ignition or throttling. To assure propellant efficiency while maintaining low production costs of hardware, we are focussed on developing engines operating at medium pressure regimes (30 – 100 bar).

 

 Our development of low cost propulsion technology is based in the following principles:

 

- simplified design of rocket engines and turbo pump units

- low level operational parameter (chamber pressures, tem­peratures, RPM of turbo pump units)

- low cost materials and manufacturing technologies

- green, low cost and easily accessible propellants

 

Due to their world wide availability in combination with no or only minor toxicity, liquid oxygen (LOX), Hydrogen Peroxide (HTP), jet propellant (JP, ‘kerosene’) or liquid methane (LCH4) are our preferred systems.

 

Please contact us for alternative propellant systems you might need.

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