An advanced two-body six-degree-of-freedom computer model employing an indeterminate structures approach has been developed for the parachute deployment process. The program determines both vehicular and decelerator responses to aerodynamic and physical property inputs. A better insight into the dynamic processes that occur during parachute deployment has been developed. The model is of value in sensitivity studies to isolate important parameters that affect the vehicular response.
An advanced technique for the prediction of decelerator system dynamics.
Aerodynamic Deceleration Systems Conference ; 1973 ; Palm Springs, CA
01.05.1973
Aufsatz (Konferenz)
Keine Angabe
Englisch
Low Density Supersonic Decelerator Parachute Decelerator System
British Library Conference Proceedings | 2013
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