Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Nissan Motor Co., Ltd.
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所報告
雑誌名(英)
Technical Report of National Aerospace Laboratory TR-907
巻
907
ページ
21
発行年
1986-06
抄録（英）
Effect of reactive stream separation on combustion performances were experimentally investigated by conducting firing tests of a N2O4/MMH propellant in a small scale combustion chamber with unlike doublet element injectors. Characteristics velocity efficiencies and specific impulses were parametrically obtained by varying the chamber pressure, the mixture ratio and the length of the combustion chamber. A distinct deterioration of the performance was observed in the region of the reactive stream separation correlated by Lawver. The most significant deterioration of the performance due to reactive stream separation occurs at a mixture ratio where otherwise the performance is at a peak.
A Study of N2O4/Amine Injector Elements Part 2 Combustion Test
naltr00907.pdf
(1.36MB)
