Feasibility study, carried out at University of Minnesota, is concerned with basic principles for design of supersonic parachute; analysis is based on shock wave patterns and area ratios related to supersonic diffuser inlet theory; several aerodynamic principles are postulated and explored which in connection with related combination of solid cone and flexible canopy lead to development of aerodynamic decelerator, called Supersonic Guide Surface Parachute.
Supersonic parachute based on inlet diffuser concept
AGARD -- Report
1963
31 pages
Report
English
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FEASIBILITY STUDY OF SHORT SUBSONIC DIFFUSER CONCEPT FOR SUPERSONIC INLET
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