並列タイトル等Performance Calculation for a Space Launch Vehicle with Air Breathing Rockets/Ramjets
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-892
一般注記Performance of a composite engine combining air breathing reockets with ramjects was calculated over the flight ranges of Mach 1.2 ～ 7, altitude 0 ～ 43 km. Based on the results of these calculations, the payload mass that could be injected into low earth orbits by a launch vehicle using such air breathing engines as a booster was estimated. The vehicle is unmanned, reusable, vertical-take-off-and-vertical-landing, having rocket engines in the base, and air breathing engines around it. The gross lift off mass of the vehicle is 155 t. The flight trajectory is generated by gravity turn only. For 200 km low earth orbit, the payload mass fraction is about 8.2％ of the gross lift off mass. Effects of various parameters used in the analysis on the payload mass fraction were also shown.
資料番号: NALTR0892000
レポート番号: NAL TR-892
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45150&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