Tungsten-rhenium alloy thermocouples to determine distribution of hydrazine-nitrogen tetroxide products within combustion chamber
Thermometric determination of oxidant-fuel distribution within a rocket combustor
1970-01-01
Miscellaneous
No indication
English
3D rocket combustor acoustics model
Tema Archive | 1992
|3D rocket combustor acoustics model
AIAA | 1992
|