@techreport{oai:jaxa.repo.nii.ac.jp:00044910,
 author = {五代, 富文 and 清水, 盛生 and 伊藤, 克弥 and 種村, 利春 and 藤原, 勉 and 日下, 和夫 and 木皿, 且人 and 佐藤, 政裕 and 高橋, 守 and 泉川, 宗男 and GODAI, Tomifumi and SHIMIZU, Morio and ITO, Katsuya and TANEMURA, Toshiharu and FUJIWARA, Tsutomu and KUSAKA, Kazuo and KISARA, Katsuto and SATO, Masahiro and TAKAHASHI, Mamoru and IZUMIKAWA, Muneo},
 month = {Feb},
 note = {300-mm-diameter thrust controllable spherical solid rocket motors with 27kg weight propellant were successfully fired under the atmospheric condition for positive extinguishment. A modified rod-in-tube grain configuration was applied in an extended spherical rocket motor for getting a neutral burning and high propellant loading fraction. Ablative material with low emissivity and low ablative temperature was applied as an insulation liner because of its desirable properties for combustion extinction. Extinguishments occured at the end of the thrust pulses during the operation time of approximately 20 seconds when the control valve of the injectant was shut down. Post-fire examination of the hardware indicated that all components were in excellent condition., 資料番号: NALTR0654000, レポート番号: NAL TR-654},
 title = {Firing Tests of Thrust Controllable Solid Rocket Motors Part II:300-mm-Diameter Spherical Grain Motors},
 year = {1981}
}