@techreport{oai:jaxa.repo.nii.ac.jp:00006009,
 author = {塚本, 太郎 and 南, 吉紀 and 山本, 行光 and 栗田, 充 and 青木, 良尚 and 石川, 和敏 and 冨田, 博史 and 元田, 敏和 and Tsukamoto, Taro and Minami, Yoshinori and Yamamoto, Yukimitsu and Kurita, Mitsuru and Aoki, Yoshihisa and Ishikawa, Kazutoshi and Tomita, Hiroshi and Motoda, Toshikazu},
 month = {Nov},
 note = {The Institute of Space Technology and Aeronautics has investigated various concepts of next generation reusable space transportation systems. Lifting-body re-entry vehicle is one of the most promising concepts among them. This type of vehicle has no wings and derives its lift solely from the shape of its body, and has the advantages of reduced structural weight, superior volumetric efficiency, and better characteristics against aerodynamic heating at hypersonic speed. On the other hand, the disadvantages of its low lift-drag ratio, poor stability and controllability at low speed makes it more difficult to land on a conventional runway than in the case of a winged vehicle like in the Automatic Landing Flight Experiment (ALFLEX), which conducted in 1996. In this report, we introduce the outline of the intended Lifting-body Flight Experiment (LIFLEX), which aims to gain the automatic landing technology using a small, low-cost system., 資料番号: AA0049500025, レポート番号: JAXA-SP-06-006},
 title = {リフティングボディ飛行実験計画について:小型制御研究機の研究},
 year = {2006}
}