Parachute design for decelerating upper atmosphere rocket probes at high altitudes, using high drag coefficients in Stokes flow regime
Development of an extremely lightweight, high- altitude decelerator
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE, 2ND ; 1968 ; EL CENTRO, CA
1969-11-01
Miscellaneous
No indication
English
High altitude decelerator systems
NTRS | 1989
|High altitude decelerator systems
AIAA | 1989
|