@techreport{oai:jaxa.repo.nii.ac.jp:00044987,
 author = {藤原, 勉 and 伊藤, 克弥 and 種村, 利春 and 清水, 盛生 and 五代, 富文 and FUJIWARA, Tsutomu and ITO, Katsuya and TANEMURA, Toshiharu and SHIMIZU, Morio and GODAI, Tomifumi},
 month = {Aug},
 note = {The X-ray television image system is used to observe the solid propellant burning surface during rocket motor operation as well as to inspect defects in solid rocket mototrs in a real time manner. This system can test 200-mm-diameter dummy propellant rocket motors with under 2 per cent discriminative capacity. Viewing of a 50-mm-diameter internal-burning rocket motor, propellant burning surface time transition and propellant burning process of the surroundings of artificial defects were satisfactorily observed. The system was demonstrated to be effective for non-destractive testing and combustion research of solid rocket motors., 資料番号: NALTR0730000, レポート番号: NAL TR-730},
 title = {X線テレビジョン透視法による固体ロケット・モータの内部観測},
 year = {1982}
}