High Drag Rotating Parachute Developed and Tested
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 November 1985
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