Paper based on studies by Space Div of Chrysler Corp proposes addition of four 120-in. solid rocket motors to Saturn IB vehicle as "Zero Stage" as attractive method of upgrading vehicle performance; Saturn IB payload capability of 40,000 lb in low earth orbit can be increased to over 78,000 lb by implementing concept; impact of Saturn IB/Zero Stage configuration on support facilities and typical schedule for implementing such program are shown.
"Zero stage" for Saturn IB launch vehicle
SAE -- Paper
SAE Meeting ; 1966
1966
19 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
A “Zero Stage” for the Saturn IB Launch Vehicle
SAE Technical Papers | 1966
|S-II stage of Saturn V launch vehicle
Engineering Index Backfile | 1964
|Engineering Index Backfile | 1964
|The S-II Stage of Saturn V Launch Vehicle
SAE Technical Papers | 1964
|The s-ii stage of saturn v launch vehicle.
NTRS | 1964
|