Supersonic and Transonic Deployment of Ribbon Parachutes at Low Altitudes-Reference-Cited by-同舟云学术

Supersonic and Transonic Deployment of Ribbon Parachutes at Low Altitudes

Published:1972-07 Issue:7 Volume:9 Page:497-502
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

MAYDEW RANDALL C.¹,JOHNSON DONALD W.¹

Affiliation:

1. Sandia Laboratories, Albuquerque, N. Mex.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.59021

Reference9 articles.

1. Aerodynamic decelerators - An engineering review

2. Pepper, W. B., Jr. "Parachute Design and Performance for Supersonic Deployment and for the Recovery of Heavy Loads,'* presented at Deutsche Gesellschaft fur Luft-und Raumfahrt E. V., Deutsche Forschungs-und Versuchsanstalt, and Advisory Group for Aerodynamic Deceleration, Technical University of Braunschweig, West Germany, Sept. 15-19, 1969

3. also SC-DC-69-1883, 1969, Sandia Labs., Albuquerque, N. Mex.

4. Recent flight-test results in deploying a 20- ft-diam ribbon parachute.

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5. Prediction of the Drag Coefficient of a 20' Conical Ribbon Parachute;Journal of Spacecraft and Rockets;1977-03