Multifunction Rocket System Development based on Advanced Hybrid Propulsion-Reference-Cited by-同舟云学术

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Multifunction Rocket System Development based on Advanced Hybrid Propulsion

Published:2016-05-13 Issue: Volume: Page:
ISSN:
Container-title:SpaceOps 2016 Conference
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Author:

Chen Yen-Sen¹,Cheng Robert¹,Chang Hao-Chi¹,Hwang Feng-Tai¹,Lai Alfred²,Lin Jhe-Wei²,Wei Shih-Sin²,Chou Tzu-Hao²,Chen Tsung-Lin²,Ho Ming-Tzu³,Wu Jong-Shinn²

Affiliation:

1. National Space Organization

2. National Chiao Tung University

3. National Cheng Kung University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2586

Reference11 articles.

1. S19 guidance of the Black Brant X sounding rocket

2. Karabeyoglu, A., Zilliac, G., Cantwell, B.J., DeZilwa, S., and Castellucci, P. "Scale-up Tests of High Regression Rate Paraffin-Based Hybrid Rocket Fuels," J. of Propulsion and Power, Voll20,No.6,p.1037-1045,2004.

Cited by 1 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. Thermodynamic Investigation of Conventional and Alternative Rocket Fuels for Aerospace Propulsion;IOP Conference Series: Materials Science and Engineering;2020-07-01

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