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規格・テクニカルリポート類

新規物質を適用した固体推進薬の理論推進性能検討

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新規物質を適用した固体推進薬の理論推進性能検討

Material type
規格・テクニカルリポート類
Author
松本, 幸太郎ほか
Publisher
宇宙航空研究開発機構(JAXA)
Publication date
2023-02-03
Material Format
Digital
Capacity, size, etc.
-
NDC
-
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Note (General):

出版タイプ: VoRIn this study, the application of novel materials to solid propellants was investigated to enhance the propulsion performance of solid rocke...

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
松本, 幸太郎
MATSUMOTO, Kotaro
Publication, Distribution, etc.
Publication Date
2023-02-03
Publication Date (W3CDTF)
2023-02-03
Alternative Title
Theoretical Propulsion Performance of Solid Rocket Propellants using Novel Materials
Periodical title
宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 令和4年度研究成果報告書
No. or year of volume/issue
JAXA-RR-22-006
Volume
JAXA-RR-22-006
Pages
29-31
ISSN (Periodical Title)
ISSN : 2433-2216
Text Language Code
jpn
Target Audience
一般
Note (General)
出版タイプ: VoR
In this study, the application of novel materials to solid propellants was investigated to enhance the propulsion performance of solid rockets. The propulsion performances of ammonium perchlorate (AP) based composite propellants contained the alternative materials was calculated by the chemical equilibrium calculations. In the case where lithium perchlorate (LP) was applied as a alternative material for the oxidizer, the vacuum specific impulse (Ispv) decreased with increasing the amount of LP, but the density specific impulse increased. The specific impulse was increased with increasing Li addition for the case where Al-Li and Al-Mg alloys were used as the metal fuel. It was also obtained that the addition of Li suppressed the formation of HCl. Although the use of Nitro-HTPB as a binder did not improve the vacuum specific impulse, it is expected to reduce the viscosity of the solid propellant slurry because it increases the ratio of the binder component at the maximum specific impulse. Therefore, the results showed that various advantages can be obtained by changing the components of AP based composite propellants to the novel materials.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA2230017007
レポート番号: JAXA-RR-22-006
Access Restrictions
インターネット公開
Data Provider (Database)
国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
Original Data Provider (Database)
宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ