並列タイトル等Liquid Injection Thrust Vector Control in High Expansion Rocket Nozzles
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-458
一般注記This paper describes an experimental study conducted on LITVC in high expansion rocket nozzles utilizing a 3kN thrust solid rocket motor. The nozzles were 15 deg conical. Freon 114B2, 70％ strontium perchlorate/water solutions and 90％ hydrogen peroxide were used as the injectant. More than thirteen different combinations of nozzle expansion ratio and injection location were tested with each injectant. All firings were conducted at the Rocket Engine High Altitude Test Facility of NAL. Main thrust, side force and yaw moment were measured by the four component thrust stand, after which the point of action of side force and main thrust augmentation were calculated. The performance of LITVC was evaluated by the moment about the center of gravity of a rocket. The effects of injectant, nozzle expansion ratio, injection location and location of the center of gravity of a rocket were illustrated.
資料番号: NALTR0458000
レポート番号: NAL TR-458
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44709&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