NASA NTRS · 19980230606
A Five-Stage Solid-Fuel Sounding-Rocket System
Abstract
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.
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Swanson, Andrew G.. 1959-03-01. A Five-Stage Solid-Fuel Sounding-Rocket System. https://ntrs.nasa.gov/citations/19980230606
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