Upper Stage Flight Experiment 10K engine design and test results

Author:

Ross R.1,Morgan D.1,Crockett D.1,Martinez L.1,Anderson W.2,McNeal C.2

Affiliation:

1. Orbital Sciences Corp., Chandler, AZ

2. NASA, Marshall Space Flight Center, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical Analyses of Thermal Protection Design in Hybrid Rocket Motors;AIAA Propulsion and Energy 2020 Forum;2020-08-17

2. Effect of dual-catalytic bed using two different catalyst sizes for hydrogen peroxide thruster;Aerospace Science and Technology;2018-07

3. Experimental Combustion Investigations from Like-Impingement Sprays of Green Propellants;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

4. Design and Ground Testing of a Hydrogen Peroxide/Kerosene Combustor for RBCC Application;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

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