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High Drag Rotating Parachute Developed and Tested

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1985

68

Abstract

A new rotating parachute designed primarily for recovery of high‐performance reentry vehicles has been developed and tested by Sandia National Laboratories in the U.S.A.

Citation

(1985), "High Drag Rotating Parachute Developed and Tested", Aircraft Engineering and Aerospace Technology, Vol. 57 No. 11, pp. 10-10. https://doi.org/10.1108/eb036185

Publisher

:

MCB UP Ltd

Copyright © 1985, MCB UP Limited

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