APOLLO Afterbody Heat Transfer and Pressure with and Without Ablation at M Infinity of 5.8 to 8.3
1966
44 pages
Report
No indication
English
Physics , Ablation , Afterbody , Apollo spacecraft , Heat transfer , Cone , Enthalpy , Mach number , Measurement , Model , Nose , Pressure , Reynolds number , Spacecraft , Stream
Ablation effects on the Apollo afterbody heat transfer.
NTRS | 1969
|Ablation effects on the Apollo afterbody heat transfer.
AIAA | 1969
|