Development of a 250 lbfv Kerosene - 90% Hydrogen Peroxide Thruster

Eric Wernimont, Dick Durant

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 2004 · 11 citations · 1 references

Concepts

Abstract

With the renewal of hydrogen peroxide usage in the last decade, many parties have become interested in usin g a non -toxic bi -propellant thruster for use in systems where weight and fast response (small impulse bit) are desired. GK has successfully developed a 250 lbfv RP -1/90% Hydrogen Peroxide thruster with very high thrust to weight and very short start times . The development test effort covers two years and test data is given from these tests.

References

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