Performance of a towed, 48-inch-diameter (121.92-cm) ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4 / by J.W. Usry.
Saved in:
| Online Access: |
Online Access |
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| Main Author: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
February 1969.
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| Series: | NASA technical note ;
D-4943. |
| Subjects: |
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