the Institute of Space and Aeronautical Science University of Tokyo
the Institute of Space and Aeronautical Science University of Tokyo
the Institute of Space and Aeronautical Science University of Tokyo
出版者
東京大学宇宙航空研究所
雑誌名
東京大学宇宙航空研究所報告
巻
2
号
2_B
ページ
613 - 621
発行年
1966-06
抄録（英）
Many fundamental testings for the heat insulation coating of SSR were done in our laboratory. Some results of our testings are available in the actual rocket. This report describes also about some results of experimental research, which are not used in actual rocket. These tests were done by the torch-burner method. This report includes mainly about the test result of graphite inpregnated by silicone oil and of epoxy resin mixed with phenolic resin powder, which shows good ablation effect, though these are not used in the actual structure of SSR-Rocket.
II.1.8 耐熱コーティング材料の実験的研究(1 機体および構造)(II.関連研究)
SA0124880.pdf
(382.06KB)
