Reference to investigation by M.VERTREGT (see Engineering Index 1955 p 917); changes in his analysis of performance of step rockets indicate that result in considering dry mass to be composed of three parts; load carrying structure, nonstructural weight, and power plant weight.
Calculation of fuel distribution in step-rockets
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 16 , n 4
1957
5 pages
Aufsatz (Zeitschrift)
Englisch
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