@techreport{oai:jaxa.repo.nii.ac.jp:00006243,
 author = {八木下, 剛 and 徳留, 真一郎 and Yagishita, Tsuyoshi and Tokudome, Shinichiro},
 month = {Jan},
 note = {In the Institute of Space and Astronautical Science (ISAS), a flight test campaign for studying reusable space transportation system has been performed with a small vehicle having a 10 kN class LOX/LH2 propulsion system. As a part of this study, we are evaluating the injector elements of reusable engine endured various thermal impacts with the small scale test pieces and original test equipment., 資料番号: AA0049056012, レポート番号: JAXA-SP-05-010},
 title = {液体酸素/液体水素エンジン噴射器の耐久性評価試験},
 year = {2006}
}