@inproceedings{oai:jaxa.repo.nii.ac.jp:00005438,
 author = {町田, 茂 and Machida, Shigeru},
 book = {宇宙航空研究開発機構特別資料: 小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告, JAXA Special Publication},
 month = {Feb},
 note = {小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館), One of the goals of the flight test with the Supersonic Experimental Airplane (NEXST-1) is to substantiate supersonic drag reduction technology with a CFD-based optimum aerodynamic design procedure. Another goal is to establish experimental flight test technology with unmanned airplane. The second flight testing of the NEXST-1 has been successfully conducted on 10 October, 2005 at Woomera Test Range, Woomera Prohibited Area, South Australia. In this report, overview of the experimental system and design and the substantiation for system requirements from flight test data are reported., 形態: カラー図版あり, 資料番号: AA0064239002, レポート番号: JAXA-SP-08-008},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ロケット実験機の飛行実験技術},
 volume = {JAXA-SP-08-008},
 year = {2009}
}