@techreport{oai:jaxa.repo.nii.ac.jp:00045058,
 author = {三谷, 徹 and 高橋, 守 and 新岡, 嵩 and 日下, 和夫 and 熊谷, 達夫 and 只野, 真 and 須藤, 孝幸 and 宮島, 博 and 斉藤, 紀男 and 丹尾, 新治 and 江口, 昭裕 and MITANI, Toru and TAKAHASHI, Mamoru and NIIOKA, Takashi and KUSAKA, Kazuo and KUMAGAI, Tatsuo and TADANO, Makoto and SUDO, Takayuki and MIYAJIMA, Hiroshi and SAITO, Norio and NIO, Shinji and EGUCHI, Akihiro},
 month = {Mar},
 note = {150mm径円筒状及び8光芒固体ロケットモータと380mm径球型ロケットモータの燃焼実験を行ない,燃焼終了後に発生する微少な残留内圧を測定した。低圧室内で測定された残留内圧は,ノズルでのガス流れを考慮して,真空におけるモータチャンバ圧に補正し,残留推力のメカニズムを詳細に検討した。これらの小さなロケットモータの実験結果に理論的検討から得られた残留推力の寸法効果を考慮して,130mm径モータ(HI-3段モータ相当)の残留推力の大きさを予測した。, Subscale rocket motors of 150mm(cylindrical) in dia.and 380mm(spherical) in dia.were tested to investigate the small residual thrust of solid propellant rockets. The residual chamber pressure was measured by using pressure gages with full ranges of 2.5 and 5 psia(0.334 and 0.668 kPa)in a high altitude simulation facility. The motor chamber pressure measured in the low pressure cell(about 3.34 kPa) was corrected to that of a vacuum. The mechanism of the residual thrust is discussed in this paper. From the scale effect of the residual thrust of a large-scale motor corresponding to the HI-3rd stage motor is predicted from the results of these experiments., 資料番号: NALTR0800000, レポート番号: NAL TR-800},
 title = {固体ロケット残留推力の実験},
 year = {1984}
}