Wind-Tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations
1960
19 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Aerodynamic characteristics , Escape capsule , Mercury project , Static stability , Aerodynamic , Axial , Capsule , Configuration , Escape , Exit , Force , Hypersonic , Mercury , Model , Modification , Moment , Normal , Pitch , Project , Stability , Static , Trim , Tunnel , Wind
Engineering Index Backfile | 1959
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