Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets-Reference-Cited by-同舟云学术

Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets

Published:2018 Issue:1 Volume:16 Page:9-18
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

SAITO Yuji¹,KIMINO Masaya¹,TSUJI Ayumu¹,OMURA Kazunobu¹,YASUKOCHI Hiroyuki²,SOEDA Kentaro²,TOTANI Tsuyoshi³,WAKITA Masashi³,NAGATA Harunori³

Affiliation:

1. Department of Space Engineering, Hokkaido University

2. Institute for Photon Science and Technology, The University of Tokyo

3. Faculty of Engineering, Hokkaido University

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/16/1/16_9/_pdf

Reference14 articles.

1. 1) Chiaverini, M J. and Kuo, K. K.: Fundamentals of Hybrid Rocket Combustion and Propulsion, AIAA, Reston, 2006, pp. 37-125.

2. 2) Whitmore, S. A., Peterson, Z. W. and Eilers, S. D.: Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor, J. Prop. Pow., 30 (2014), pp. 78-86.

3. 3) Karabeyoglu A., Toson E. and Evans B.: O/F shift in Hybrid Rockets, 50th AIAA/SAE/ASEE Joint Propulsion Conference, Cleveland, U.S.A., AIAA 2014-3851, 2014.

4. 4) Nagata, H., Okada, K. Sanda, T., Kato, T., Akiba, R., Satori, S. and Kudo, I.: Combustion Characteristics of Fibrous Fuels for Dry Towel Hybrid Rocket Motor, The Journal of Space Technology and Science, 13 (1997), pp.11-16.

5. 5) Kato, T., Hashimoto, N., Nagata, H., Akiba, R. and Kudo, I.: A preliminary study of end-burning Hybrid Rocket, Part 1: Combustion Stability, JSASS, 49 (2001), pp. 33-39 (in Japanese).

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3. Response Mechanisms in Axial-Injection End-Burning Hybrid Rockets;AIAA Propulsion and Energy 2019 Forum;2019-08-16

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