@techreport{oai:jaxa.repo.nii.ac.jp:00002482,
 author = {小林, 宙 and 飯島, 朋子 and 西沢, 啓 and Kobayashi, Hiroshi and Iijima, Tomoko and Nishizawa, Akira},
 month = {Mar},
 note = {The Japan Aerospace Exploration Agency (JAXA) is planning flight demonstration of an electric propulsion system which is equipped with new functions using a motor glider on 2014. The new electric propulsion system will be converted form the existing reciprocating engine of motor glider and be installed with motor glider. Prior to the development of the electric propulsion system, flight tests are conducted to acquire performance of JA07TTCECO with original propulsion system. Based on these flight test result, determined specifications of the electric propulsion system for replacing original system are as follows, 1)Take-off Power(max 150s):60kW, 2)Maximum Propeller Speed:2300rpm, 3)Maximum Ambient Temperature:40 C, 4)Maximum Continuous Power:32kW., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530008000, レポート番号: JAXA-RM-14-005},
 title = {原型機飛行試験による航空機用電動推進系の仕様検討},
 year = {2015}
}