Accession Number:

AD0431321

Title:

A SUPERSONIC PARACHUTE BASED ON THE INLET DIFFUSER CONCEPT,

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1963-04-01

Pagination or Media Count:

31.0

Abstract:

Several aerodynamic principles are postulated and explored which, in connection with a related combination of a solid cone and a flexible canopy lead to the development of an aerodynamic decelerator, called the supersonic guide surface parachute. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE