@techreport{oai:jaxa.repo.nii.ac.jp:00006007,
 author = {佐藤, 哲也 and Sato, Tetsuya},
 month = {Nov},
 note = {The Japan Space Exploration Agency (JAXA) is developing a hypersonic turbojet engine to realize Mach 5 or 6 cruise vehicles and reusable LEO transportation systems. Design and fabrication of a subscale turbojet engine of 1 kN thrust with an air precooking system have been continued. In 2005, we conducted performance verification test of a newly developed air-precooler, compressor, and a liquid hydrogen supply system for the subscale engine. Test results are briefly reported in this paper., 資料番号: AA0049500023, レポート番号: JAXA-SP-06-006},
 title = {飛行実験をめざした極超音速ターボジェットエンジンの開発状況},
 year = {2006}
}