Results Of A Free Flight Test To Determine The Performance Characteristics Of A Towed Conical Decelerator
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Author | : J. W. Usry |
Publisher | : |
Total Pages | : 48 |
Release | : 1969 |
Genre | : Results of a Free-Flight Test to Determine the Performance Characteristics of a Towed, Conical Decelerator |
ISBN | : |
An inflatable fabric decelerator was tested in free flight to determine its drag and stability characteristics. The inflated decelerator approximated an 80 cone with a 48 inch (121.9) base and was towed behind a cone cylinder flare payload at a distance of 13.6 feet (4.15 m) from payload base.
Author | : |
Publisher | : |
Total Pages | : 694 |
Release | : 1969 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 966 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 436 |
Release | : 1968 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 956 |
Release | : 1970 |
Genre | : Science |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 604 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 128 |
Release | : 1963 |
Genre | : Astronautics |
ISBN | : |
Author | : E. G. Ewing |
Publisher | : |
Total Pages | : 502 |
Release | : 1979 |
Genre | : Parachutes |
ISBN | : |
This document serves as the third revision of the USAF Parachute Handbook which was first published in 1951. The data and information represent the current state of the art relative to recovery system design and development. The initial chapters describe representative recovery applications, components, subsystems, material, manufacture and testing. The final chapters provide empirical data and analytical methods useful for predicting performance and presenting a definitive design of selected components into a reliable recovery system.
Author | : |
Publisher | : |
Total Pages | : 510 |
Release | : 1984 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1320 |
Release | : 1966 |
Genre | : Government publications |
ISBN | : |