並列タイトル等N2O4/アミン インジェクタエレメントの実験 その2 燃焼試験結果
タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-907
一般注記Effect of reactive stream separation on combustion performances were experimentally investigated by conducting firing tests of a N2O4/MMH propellant in a small scale combustion chamber with unlike doublet element injectors. Characteristics velocity efficiencies and specific impulses were parametrically obtained by varying the chamber pressure, the mixture ratio and the length of the combustion chamber. A distinct deterioration of the performance was observed in the region of the reactive stream separation correlated by Lawver. The most significant deterioration of the performance due to reactive stream separation occurs at a mixture ratio where otherwise the performance is at a peak.
資料番号: NALTR0907000
レポート番号: NAL TR-907
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45166&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース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