Hybrid Propulsion Technology Development in Japan for Economic Space Launch-Reference-Cited by-同舟云学术

Hybrid Propulsion Technology Development in Japan for Economic Space Launch

Published:2016-08-20 Issue: Volume: Page:545-575
ISSN:1869-1730
Container-title:Chemical Rocket Propulsion
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Author:

Shimada Toru,Yuasa Saburo,Nagata Harunori,Aso Shigeru,Nakagawa Ichiro,Sawada Keisuke,Hori Keiichi,Kanazaki Masahiro,Chiba Kazuhisa,Sakurai Takashi,Morita Takakazu,Kitagawa Koki,Wada Yutaka,Nakata Daisuke,Motoe Mikiro,Funami Yuki,Ozawa Kohei,Usuki Tomoaki

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-27748-6_22

Reference55 articles.

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2. Japan Space Systems and CSP Japan, Inc. private communication

3. Garvey Spacecraft Corporation (2012) Incremental evolution of a 10/250 NLV into a 20/450 NMSLV, Small Business Innovation Research 2012, 12-1 E1.02-9091. http://sbir.gsfc.nasa.gov/SBIR/abstracts/12/sbirselect/phase1/SBIR-12-1-S-E1.02-9091.html

4. Rocketdyne A (2013) Spartan nano-launch vehicle. In: 16th US Space and Missile Defense symposium. http://smdsymposium.org/wpcontent/uploads/2013/09/Kaufman-Nano-Launch-Vehicle-presentation.pdf

5. USASMDC/ARSTRAT, SWORDS. http://www.smdc.army.mil/FactSheets/SWORDS.pdf

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