@techreport{oai:jaxa.repo.nii.ac.jp:00043878,
 author = {楢崎, 哲二 and 荻原, 裟千男 and 吉原, 正一 and NARASAKI, Tetsuji and OGIWARA, Sachio and YOSHIWARA, Shoichi},
 month = {Mar},
 note = {Graphs showing characteristic curves of rocket propellants performance (Isp,C*,T,etc.),are available to assist the design or investigation of rocket engines.As the most practical or most used liquid rocket propellants,four propellants(LOX-LH2,N204-A・50,LOX-RP・1,LOX-C2H5OH)were selected,and the extent of practical usage performance of the propellants were computed(ε,Pc,O/F).The results are shown in the respective graphs., 資料番号: NALTM0295000, レポート番号: NAL TM-295},
 title = {液体ロケット推進薬の性能特性図},
 year = {1975}
}