@techreport{oai:jaxa.repo.nii.ac.jp:00044985,
 author = {鎮西, 信夫 and 升谷, 五郎 and 小室, 智幸 and 工藤, 賢司 and 村上, 淳郎 and 石井, 進一 and CHINZEI, Nobuo and MASUYA, Goro and KOMURO, Tomoyuki and KUDO, Kenji and MURAKAMI, Atsuo and ISHII, Shinichi},
 month = {Aug},
 note = {An experimental study on air breathing rockets utilizing rockets with multi-nozzles was conducted for the purpose of reducing the length of the secondary combustor. Two kinds of multi-nozzles, one consisting of four and the other of seven nozzles, were used. The measurements include radial distributions of Pitot pressure and gas composition at the secondary combustor exit, axial wall pressure distribution, and air stagnation pressure. The results were compared with those previously obtained in an experiment using a single nozzle, and the influence of number of nozzles, N, on the relation between length and performance of the secondary combustor was investigated. Despite the distortion of the individual exhaust jets from the multi-nozzle, combustor length for sufficient performance was found to be proportional to the diameter of rocket nozzle exit or 1/the root N., 資料番号: NALTR0728000, レポート番号: NAL TR-728},
 title = {空気吸込式ロケットの研究(II)-ロケットノズル数の影響-},
 year = {1982}
}