Application of Low Melting Point Thermoplastics to Hybrid Rocket Fuel-Reference-Cited by-同舟云学术

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Application of Low Melting Point Thermoplastics to Hybrid Rocket Fuel

Published:2012 Issue:ists28 Volume:10 Page:Pa_1-Pa_5
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:

WADA Yutaka,JIKEI Mitsutoshi,KATO Ryuichi,KATO Nobuji,HORI Keiichi

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/10/ists28/10_ists28_Pa_1/_pdf

Reference1 articles.

1. *

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Performance Comparison of Paraffin/Ethanol Fuel Blends in a Laboratory-Scale Hybrid Rocket Motor;Journal of Propulsion and Power;2023-09

2. Experimental Investigation of a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine Using Low-Melting-Point Thermoplastic Fuel and Oxygen;Aerospace;2023-08-15

3. Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket Engines;Aerotecnica Missili & Spazio;2022-05-24

4. Conceptual Study on Low-Melting-Point Thermoplastic Fuel/Nitrous Oxide Hybrid Rockoon;Journal of Spacecraft and Rockets;2022-01

5. IMPROVEMENT OF COMBUSTION EFFICIENCY USING A BAFFLE PLATE FOR A LT/GOX HYBRID ROCKET MOTOR;International Journal of Energetic Materials and Chemical Propulsion;2019

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