The objective of this program is to advance the state of the art by using analytical and engineering techniques for designing aerodynamic deployable decelerators. Three classes of decelerators - small supersonic parachutes, ram-air-inflated BALLUTEs, and large high-dynamic-pressure parachutes were investigated. Free-flight tests using a newly developed GAC missile system and wind-tunnel tests in the full-scale propulsion wind-tunnel facility at Arnold Research Center were conducted. The results indicated that the engineering techniques that were developed led to improved decelerators and that an improved free-flight test capability was established. (Author)
Aerodynamic Deployable Decelerator Performance - Evaluation Program
1965
305 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Astronautics , Space capsules , Manned spacecraft , Deceleration , Recovery , Feasibility studies , Deployment , Design , Rescues , Inflatable structures , Wind tunnel models , Model tests , Parawings , Balloons , Supersonic characteristics , Drag , High altitude , Aerodynamic heating , Ablation , Aerodynamic characteristics , Nose cones , Reentry vehicles , Free fall models , Ribbon parachutes , Spin recovery parachutes , Thermodynamics , Heat shields , Payload , Ballutes , Space rescue