Numerical Analysis on Axial Force Characteristics of Reusable Launch Vehicle at 150–180° Angles of Attack-Reference-Cited by-同舟云学术

Numerical Analysis on Axial Force Characteristics of Reusable Launch Vehicle at 150–180° Angles of Attack

Published:2023 Issue:4 Volume:66 Page:118-129
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:

MAMASHITA Tomohiro¹,MUTO Tomotaro²,KITAMURA Keiichi¹,NONAKA Satoshi³

Affiliation:

1. Department of Mechanical, Materials, and Ocean Engineering, Yokohama National University

2. Department of Aeronautics and Astronautics, The University of Tokyo

3. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/66/4/66_T-22-10/_pdf

Reference21 articles.

1. 1) Ogawa, H., Nonaka, S., and Inatani, Y.: A Concept and Its Aerodynamic Design of a Sub-Orbital Reusable Rocket, AIAA Paper 2004-2538, 2004.

2. 2) Ogawa, H., Nonaka, S., Naruo, Y., Ito, T., and Inatani, Y.: Reusable Sounding Rocket, Int. J. Microgravity Sci. Appl., 33 (2016), pp. 330303-1–330303-5.

3. 3) Kimura, T., Hashimoto, T., Sato, M., Takada, S., Moriya, S., Yagishita, T., Naruo, Y., Ogawa, H., Ito, T., Obase, K., and Ohmura, H.: Reusable Rocket Engine: Firing Tests and Lifetime Analysis of Combustion Chamber, J. Propuls. Power, 32 (2016), pp. 1087–1094.

4. 4) Nonaka, S.: Recent Progress of Reusable Vehicle Testing, 5th Space Solar Power Systems Symposium, 2020, pp. 86–92 (in Japanese).

5. 5) Nonaka, S., Nakamura, T., and Inatani, Y.: Aerodynamics for Reusable Rocket in Its Returning Flight, 48th Fluid Dynamics Conference/34th Aerospace Numerical Simulation Symposium, Ishikawa, Japan, JSASS-2016-2103-A, 2016 (in Japanese).