@article{oai:jaxa.repo.nii.ac.jp:00033017,
 author = {矢島, 信之 and 太田, 茂雄 and 秋山, 弘光 and 岡部, 選司 and 西村, 純 and 橋本, 保成 and 川口, 淳一郎 and YAJIMA, Nobuyuki and OHTA, Shigeo and AKIYAMA, Hiromitsu and OKABE, Yorigi and NISHIMURA, Jun and HASHIMOTO, Yasunari and KAWAGUCHI, Junichiro},
 journal = {宇宙科学研究所報告. 特集: 大気球研究報告},
 month = {Nov},
 note = {An azimuth control system using N_2 gas thruster (S-J control system) has been developed and employed for the quick and steady control of a large and heavy balloon gondola. In the gondola, a winged space vehicle and a booster rocket are to be installed for its re-entry flight test. When the balloon reaches ceiling altitude, the gondola is oriented to the required direction by using the S-J control system and then the vehicle is released from the gondola. A preliminary flight test has been carried out to test the S-J control system and a separation mechanism of the vehicle at Sanriku Balloon Center in May 1987. The experimental results show that this control system is applicable for the actual re-entry flight test of the winged space vehicle., 資料番号: SA0166861000},
 pages = {27--42},
 title = {ガスジェットによる大型ゴンドラの方向制御},
 volume = {22},
 year = {1988}
}