Influence of Chemical Composition on Physical Properties of Low-Melting-Point Thermoplastics for Hybrid Rocket Fuel-Reference-Cited by-同舟云学术

Influence of Chemical Composition on Physical Properties of Low-Melting-Point Thermoplastics for Hybrid Rocket Fuel

Published:2021 Issue:2 Volume:19 Page:238-244
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:

KAWABATA Yo¹,WADA Yutaka²,YASUDA Takeshi³,KATO Ryuichi⁴,KATO Nobuji⁵,HORI Keiichi⁶,NAGASE Ryo²

Affiliation:

1. Department of Mechanical Engineering, Fukuoka University

2. Department of Innovative Mechanical and Electronic Engineering, Chiba Institute of Technology

3. Tokyo Metropolitan Industrial Technology Research Institute

4. Akita University

5. Katazen Corporation

6. Institute of Space and Astronautical Science, JAXA

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/19/2/19_19.238/_pdf

Reference15 articles.

1. 1) National aeronautics and space administration: Solid Propellant Grain Structural Integrity Analysis, NASA SP-8073, 1973.

2. 2) Strand, L., Jones, M., Ray, R., and Cohen. N.: Characterization of Hybrid Rocket Internal Heat Flux and HTPB fuel pyrolysis, AIAA Paper 94-2876, 1994.

3. 3) Karabeyoglu, M. A., Cantwell, B. J., and Altman, D.: Development and Testing of Paraffin-based Hybrid Rocket Fuels, AIAA Paper 2001-4503, 2001.

4. 4) Wada, Y., Jikei, M., Kato, R., Kato, N., and Hori, K.: Application of Low Melting Point Thermoplastics to Hybrid Rocket Fuel, Trans. JSASS, Aerospace Technology Japan, 10, ists28 (2012), pp. 1–5.

5. 5) Wada, Y., Kato, R., Kato, N., and Hori, K.: Small Rocket Launch Experiment Using Low Melting Point Temperature Thermoplastic Fuel/N2O Hybrid Rocket, AIAA Paper 2013-5050, 2013.