@techreport{oai:jaxa.repo.nii.ac.jp:00043787,
 author = {五代, 富文 and 岡部, 裕二郎 and 清水, 昭紀 and 伊藤, 克弥 and 西村, 久男 and GODAI, Tomifumi and OKABE, Yujiro and SHIMIZU, Shoki and ITO, Katsuya and NISHIMURA, Hisao},
 month = {Jun},
 note = {An accurate and standard specific impulse measurement system with an overall error not exceeding 0.1% for solid rocket propellants is described. After investigating a con- ventional specific impulse measurement system existing at the National Aerospace Laboratory, some new design concepts, consideration of ballistic evaluation of a solid rocket motor, an accurate thrust stand, and electronic equipment and environmental conditions are discussed. The results of system tests, static calibration and motor firing tests are also described., 資料番号: NALTM0203000, レポート番号: NAL TM-203},
 title = {固体ロケットの比推力測定の標準化},
 year = {1971}
}