Dornier-System GmbH proposed development of radio-controlled recoverable and reusable sounding rocket, to reduce expense of experiments; requirements of recovery system for ballistic missiles and considerations which led to system using paraglider, having relatively high position of center of gravity; equipment consists of frame with two profiled aluminum rails, accommodating, flush with outer surface, paraglider beams with rolled-up fabric and nose and stern bulkheads; fitted to frame is fuselage shell, cylindrical stern body and nose cone; paraglider is deployed by means of pneumatic system in beam beds; flight tests and flight stability criteria and future projects.
New recovery system for sounding rockets
Spaceflight
Spaceflight ; 9 , n 2
1967
5 pages
Article (Journal)
English
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Recovery System for Sounding Rockets
NTIS | 1971
|NTRS | 1965
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1959
|NTIS | 2024
|TIBKAT | 1959
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