A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude of 525 nautical miles and that of 100 pounds to 300 nautical miles is described. Data obtained from a typical flight test of the system are discussed.
Five-Stage Solid-Fuel Sounding-Rocket System
1959
26 pages
Report
No indication
English
Five-stage solid-fuel sounding-rocket system
Engineering Index Backfile | 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
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