Techniques available which determine optimum sounding rocket capability as function of fuels and materials limitations, for types of multistaged rockets which are of greatest importance with respect to space flight; calculation results presented for two examples representing extreme altitude sounding to summit height of one earth diameter, and minimal lunar flight.
Ultimate design of high altitude sounding rockets
Jet Propulsion
Jet Propulsion ; 27 , n 10
1957
2 pages
Article (Journal)
English
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