Design and Development Testing of the TR108 - a 30Klbf-Thrust-Class Hydrogen Peroxide / Hydrocarbon Pump-Fed Engine
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American Institute of Aeronautics and Astronautics
Reference3 articles.
1. 1Dressler, G. A., and Bauer, J. M. "TRW Pintle Engine Heritage and Performance Characteristics," AIAA-2000-3871, 36thAIAA/ASME/SAE/ASEE JointPropulsion Conference andExhibit, Huntsville,AL, July 2000.
2. 3Calvignac, J., Dang, L., Tramel, T. L., and Paseur, L. "Design and Testing of Non-Toxic RCS Thrusters for Second Generation Reusable Launch Vehicles," AIAA-2003-4922, 39thAIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2003.
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