The paper is devoted to the study of the possibility to use the flat perforated stabilizing devices as an alternative to lattice stabilizers of the separation unit in the case of the spacecraft emergency escape system activation. The aerodynamic characteristics and flow structures of the model with solid and perforated stabilizers were analyzed.
Application of Perforated Stabilizers for Static Stability at Subsonic Flight Speeds of the Separation Unit of a Spacecraft Emergency Escape System
Russ. Aeronaut.
Russian Aeronautics ; 65 , 4 ; 655-661
2022-10-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Flight research at high subsonic speeds
Engineering Index Backfile | 1948
|Airfoil shape for flight at subsonic speeds
NTRS | 1976
|