@techreport{oai:jaxa.repo.nii.ac.jp:00044709,
 author = {升谷, 五郎 and 鎮西, 信夫 and 石井, 進一 and 工藤, 賢司 and 小室, 智幸 and MASUYA, Goro and CHINZEI, NOBUO and ISHII, Shinichi and KUDO, Kenji and KOMURO, Tomoyuki},
 month = {May},
 note = {This paper describes an experimental study conducted on LITVC in high expansion rocket nozzles utilizing a 3kN thrust solid rocket motor. The nozzles were 15 deg conical. Freon 114B2, 70％ strontium perchlorate/water solutions and 90％ hydrogen peroxide were used as the injectant. More than thirteen different combinations of nozzle expansion ratio and injection location were tested with each injectant. All firings were conducted at the Rocket Engine High Altitude Test Facility of NAL. Main thrust, side force and yaw moment were measured by the four component thrust stand, after which the point of action of side force and main thrust augmentation were calculated. The performance of LITVC was evaluated by the moment about the center of gravity of a rocket. The effects of injectant, nozzle expansion ratio, injection location and location of the center of gravity of a rocket were illustrated., 資料番号: NALTR0458000, レポート番号: NAL TR-458},
 title = {高膨張ノズル内の液体二次噴射推力方向制御},
 year = {1976}
}