Multidisciplinary Design Optimization of a Two-Stage-to-Orbit Reusable Launch Vehicle with Ethanol-Fueled Rocket-Based Combined Cycle Engines-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization of a Two-Stage-to-Orbit Reusable Launch Vehicle with Ethanol-Fueled Rocket-Based Combined Cycle Engines

Published:2017 Issue:5 Volume:60 Page:265-275
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:

FUJIKAWA Takahiro¹,TSUCHIYA Takeshi¹,TOMIOKA Sadatake²

Affiliation:

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

2. Kakuda Space Center, 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/60/5/60_T-15-71/_pdf

Reference27 articles.

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2. 2) Tani, K., Tomioka, S., Kato, K., Ueda, S., and Takegoshi, M.: Recent Activities in Research of the Combined Cycle Engine at JAXA, Trans. JSASS Aerospace Technology Japan, 8, ists27 (2010), pp. Ta_1–Ta_6.

3. 3) Tomioka, S., Hiraiwa, T., Saito, T., Kato, K., Kodera, M., and Tani, K.: System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle, Trans. JSASS Aerospace Technology Japan, 12, ists29 (2014), pp. Pa_91–Pa_99.

4. 4) Kodera, M., Ogawa, H., Tomioka, S., and Ueda, S.: Multi-Objective Design and Trajectory Optimization of Space Transportation Systems with RBCC Propulsion via Evolutionary Algorithms and Pseudospectral Methods, AIAA Paper 2014-629, 2014.

5. 5) Ogawa, H., Kodera, M., Tomioka, S., and Ueda, S.: Multi-Phase Trajectory Optimization for Access-to-Space with RBCC-Powered TSTO via Surrogate-Assisted Hybrid Evolutionary Algorithms Incorporating Pseudo-Spectral Methods, AIAA Paper 2014-2360, 2014.

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