Semianalytic method derived for calculating range of 1-stage, ballistic, rocket propelled, surface-to-surface missiles; method consists of obtaining certain analytic solutions, supposing flight in vacuum, and then correcting these solutions for effect of drag; results presented as working formulas and plots suitable for use in preliminary design studies.
Ballistic missile performance
Jet Propulsion
Jet Propulsion ; 26 , n 4
1956
5 pages
Article (Journal)
English
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