@techreport{oai:jaxa.repo.nii.ac.jp:00044480,
 author = {河崎, 俊夫 and 塙, 武敏 and 斎藤, 秀夫 and 高島, 一明 and 河本, 巌 and KAWASAKI, Toshio and HANAWA, Taketoshi and SAITO, Hideo and TAKASHIMA, Kazuaki and KAWAMOTO, Iwao},
 month = {Jul},
 note = {Free Flight Model FFM-10 is a model which simulates a supersonic aircraft with delta wing. The model is propelled by a rocket motor installed in the fuselage. Longitudinal short period motion is excited by two side-jets ignited in sequence. Measurements of acceleration in the direction of pitching motion enable the determination of longitudinal static and dynamic aerodynamic derivatives. The results are compared with theoretical estimates and show fairly food agreement. Although much improvement should be pursued to obtain satisfactory accuracy, the preliminary results show that the technique employed is very promising., 資料番号: NALTR0237000, レポート番号: NAL TR-237},
 title = {自由飛行模型FFM-10による縦の動安定特性の飛しょう実験},
 year = {1971}
}