Wind-Tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster

1960

16 pages

Report

Keine Angabe

Englisch

Manned Spacecraft , Aerodynamic characteristics , Nonlifting vehicle , Reentry body , Static stability , Aerodynamic , Alloy , Aluminum , Angle , Attack , Body , Booster , Booster rocket , Capsule , Configuration , Escape , Model , Nonlifting , Reentry , Rocket , Stability , Static , Subsonic , Tower , Transonic , Tunnel , Vehicle , Wind