2026-03-15T18:06:11Z https://jaxa.repo.nii.ac.jp/oai

oai:jaxa.repo.nii.ac.jp:00049466 2023-06-20T18:32:10Z 1543:1693:2270 1887:1891

トータルインパルス 100kN･ s級ハイブリッドロケットの打ち上げ試験と飛行シミュレーション Total Impulse 100kNs Class Hybrid Rocket and Flight Simulation ウイ, ヤンイ 高野, 敦 喜多村, 竜太 OOI, Yenyi TAKANO, Atsushi KITAMURA, Ryuta 令和4年度宇宙輸送シンポジウム（2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)) , 相模原市, 神奈川県 Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan The flight simulation before launching was done by using data from wind forecast. The plan was use one wind data of the past for the flight simulation and got a prediction of highest height achieve at 23km, but during the flight test by using the data from wind forecast to simulate the area of falling, we had to drop the angle of launch from 85° at the beginning to 72°, the prediction of highest height achieve drops from 22km to 4km to make it fall into the area planned. After the flight test, highest height achieved was 3.7km, which was lower than expected, so another flight simulation with reconsideration for the drag coefficient is needed. 資料番号: SA6000184010 STCP-2022-010 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS) 2023-01 jpn conference paper AM https://jaxa.repo.nii.ac.jp/records/49466 令和4年度宇宙輸送シンポジウム: 講演集録 Proceedings of Space Transportation Symposium FY2022 https://jaxa.repo.nii.ac.jp/record/49466/files/SA6000184010.pdf application/pdf 661.1 kB 2023-05-23