Consideration of Mechanical Properties of Solid Propellants in Low Temperature Environments for Application to Planetary Exploration

Hiroshi Tabata

講演情報

Oral Session

a) Chemical Propulsion and Air-breathing Engines

[a-5] Solid Rocket 2

2023年6月7日(水) 11:00 〜 12:00 The large Meeting Room 1 5F (The large Meeting Room 1 5F)

Jouke Hijlkema (ONERA),Apollo B. Fukuchi (Saitama Institute of Technology)

11:00 〜 11:20

[2023-a-18] Consideration of Mechanical Properties of Solid Propellants in Low Temperature Environments for Application to Planetary Exploration

*Hiroshi Tabata¹, Akihiro Terachi¹, Sumika Shimokoshi², Ryuga Itaki², Akihiro Iwasaki³, Soichiro Yamaguchi² (1. Kansai Univ. Department of Science and Engneering, 2. Kansai Univ. Department of Pure and Applied Physics, 3. Yspace Inc.)

キーワード：Composite Propellant, Glass Transition, TMA, Mechanical Properties