Development of a pressure-fed rocket engine using hydrogen peroxide and JP-8

Author:

Wu P.-K.1,Fuller R.1,Morlan P.1,Ruttle D.1,Nejad A.1,Anderson W.2

Affiliation:

1. Kaiser Marquardt, Van Nuys, CA

2. Orbital Sciences Corp., Chandler, AZ

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. Effects of Transverse Jet Penetration on High-Test Peroxide/Kerosene Bipropellant Thruster;Journal of Propulsion and Power;2018-05

2. Experimental Characterization of Advanced Materials for the Catalytic Decomposition of Hydrogen Peroxide;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Development of Hydrogen Peroxide Monopropellant Rockets;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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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