博士論文

自己加圧式ロケットエンジン用液体推進剤の流動特性に関する研究

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自己加圧式ロケットエンジン用液体推進剤の流動特性に関する研究

Persistent ID (NDL)
info:ndljp/pid/13122652
Material type
博士論文
Author
安田, 一貴
Publisher
-
Publication date
2021-03-23
Material Format
Digital
Capacity, size, etc.
-
Name of awarding university/degree
室蘭工業大学,博士(工学)
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Detailed bibliographic record

Summary, etc.:

航空宇宙産業の発展に伴い,推進系の小型,軽量,簡素化が求められている.これらの需要に応える選択肢の一つに,亜酸化窒素の推進剤利用が挙げられる.亜酸化窒素は,常温で高い飽和蒸気圧を有することから,別途加圧システムを必要せず自己加圧供給が可能であるほか,常温で液体として取り扱うことができる.これらの特長...

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  • 2024-01-19 再収集

  • 2024-01-19 再収集

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Digital

Material Type
博士論文
Author/Editor
安田, 一貴
Author Heading
Publication Date
2021-03-23
Publication Date (W3CDTF)
2021-03-23
Degree grantor/type
室蘭工業大学
Date Granted
2021-03-23
Date Granted (W3CDTF)
2021-03-23
Dissertation Number
甲第467号