Conceptual Design Model of High-Altitude Test Stand for Rocket Engines-Reference-Cited by-同舟云学术

Conceptual Design Model of High-Altitude Test Stand for Rocket Engines

Published:2016 Issue:3 Volume:59 Page:161-169
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

KANDA Takeshi¹,OGAWA Yohei¹,SUGIMORI Daizo²,KOJIMA Makoto¹

Affiliation:

1. Research and Development Directorate, JAXA

2. Space Technology Directorate I, JAXA

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/59/3/59_T-15-54/_pdf

Reference27 articles.

1. 1) JAXA Kakuda Space Center, http://www.kspc.jaxa.jp/japanese/index.html (accessed June 16, 2015)

2. 2) Maynard, B. T. and Raines, N.: Altitude Testing of Large Liquid Propellant Engines, AIAA Paper 2008-3700, Seattle, Washington, USA, June 2008.

3. 3) Harris, D. and Cort, R.: White Sands Test Facility Test Stand 401, AIAA Paper 98-4009, Cleveland, OH, USA, 1998.

4. 4) Kenzakowski, D. C. and Brinckman, K. W.: CFD Simulation of NASA B-2 Spray Chamber during Rocket Fire, AIAA Paper 2008-0790, Reno, NV, Jan. 2008.

5. 5) Schäfer, K. and Zimmermann, H.: Simulation of Flight Condition during Lift OFF for Rocket Engine Testing, AIAA Paper 2004-4001, Fort Lauderdale, FL, USA, July 2004.

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