Author:
Zhang Jiaqi,Wang Ke,Chen Lanwei
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference40 articles.
1. Tom Hunsaker, Matt Bille, Paul Kolodziejski, Nanosat launch vehicles: a global perspective and business case, in: 2013 AIAA SPACE Forum, AIAA 2013-3353.
2. Eric Hurlbert, Robert Morehead, John C. Melcher, Matt Atwell, Integrated pressure-fed liquid oxygen/methane propulsion systems –morpheus experience, MARE, and future applications, in: 52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA 2016-4681.
3. Two-phase flow characteristics of liquid oxygen flow in low pressure liquid rocket engine;Cho;Cryogenics,2004
4. J. Collins, E. Hurlbert, K. Roming, et al., Sea level flight demonstration & altitude characterization of a LO2/LCH4 based ascent propulsion lander, in: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2009-4948.
5. System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump;Cui;Acta Astronaut.,2020
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