@techreport{oai:jaxa.repo.nii.ac.jp:00044784,
 author = {泉川, 宗男 and 高橋, 守 and 三谷, 徹 and 新岡, 嵩 and IZUMIKAWA, Muneo and TAKAHASHI, Mamoru and MITANI, Tohru and NIIOKA, Takashi},
 month = {Mar},
 note = {Spinning combustion tests for a 200mm-dia. class solid propellant rocket were conducted and compared with numerical results. The combustion surface obtained by the extinction test shows that the acceleration-produced burning effect is limited to the region having the angle 85.5 deg to 90 deg between the combustion surface and the acceleration vector. This angle extent was independent of the burning time and the grain configuration. The aspects of the combustion surface, together with the transient burning-rate augmentation data given by the strand experiment, were included in a model for computer programming of the predicted pressure-time diagram. The predicted pressure history and the variation of grain configuration with time show a qualitatively good comparison., 資料番号: NALTR0530000, レポート番号: NAL TR-530},
 title = {200mm径固体ロケットのスピン燃焼実験},
 year = {1978}
}