@techreport{oai:jaxa.repo.nii.ac.jp:00002762,
 author = {荒井, 功恵 and 臼杵, 茂 and 今村, 裕志 and 柳, 英二 and Arai, Katsuyoshi and Usuki, Shigeru and Imamura, Hiroshi and Yanagi, Eiji},
 month = {Feb},
 note = {Tsubasa (MDS-1) was launched by H-2A launch vehicle TF-2 on Feb 4th 2002. Tsubasa exceeded the planned 1-year orbit mission life. To satisfy the short term, low cost and reliable satellite, new technology and approach are applied for Tsubasa system. This paper describes the new technologies of Tsubasa bus development, the evaluation of each approach and comparison with NASA LEWIS satellite., 資料番号: AA0046975002, レポート番号: JAXA-RM-03-022},
 title = {つばさ(MDS-1)バス開発手法},
 year = {2004}
}