Details of rocket capable of carrying sounding probes and payloads of 25 and 100 lb to altitudes of 525 and 300 nautical mi, respectively; data obtained from typical flight test of system.
Five-stage solid-fuel sounding-rocket system
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 3-6-59L
1959
22 pages
Report
Englisch
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Five-Stage Solid-Fuel Sounding-Rocket System
NTIS | 1959
|A Five-Stage Solid-Fuel Sounding-Rocket System
NTRS | 1959
|Two-stage sounding rocket problem
Engineering Index Backfile | 1967
|The Two-Stage Sounding-Rocket Problem
NTIS | 1967
|The two-stage sounding rocket problem.
AIAA | 1967
|