Apollo afterbody heat transfer and pressure with and without ablation at Mach numbers 5.8 - 8.3
Apollo afterbody heat transfer and pressure with and without ablation at M infinity of 5.8 to 8.3
1966-09-01
Miscellaneous
No indication
English
Ablation effects on the Apollo afterbody heat transfer.
NTRS | 1969
|Ablation effects on the Apollo afterbody heat transfer.
AIAA | 1969
|