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-998
一般注記A new technique using a strand burner was developed to investigate the combustion efficiency of metals in solid propellants. A strand of propellants was burned under a given pressure and all reactants and products were trapped in the closed vessel. Condensed and gaseous species were analyzed quantitatively using various titration methods and gas-chromatography. The results derived from the strand burner were compared with the ηc evaluated from firing tests of subscale motors. The combustion efficiency of Al and B in various propellants was measured. A combustion model for metal powders including agglomeration, ignition and steady burning of particles was investigated. Effects of B/Al ratios and particle size of B on the combustion efficiency of propellants containing Al and B were discussed based on the combustion model.
資料番号: NALTR0998000
レポート番号: NAL TR-998
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