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A Five-Stage Solid-Fuel Sounding-Rocket SystemA 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.
Document ID
19980230606
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Swanson, Andrew G. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1959
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-MEMO-3-6-59L
Report Number: NASA-MEMO-3-6-59L
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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