Static aerodynamic characteristics of experimental nonlifting reentry capsule in combination with rocket booster at Mach numbers from 0.60 to 1.20
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
1960-09-01
Report
No indication
English
Engineering Index Backfile | 1959
|Wind-Tunnel Tests on Aerodynamic Characteristics of EXPRESS Reentry Capsule
British Library Conference Proceedings | 1994
|