To meet the SATURN IB requirements, the thrust of the first stage engine, the H-l, was increased from 188, 000 to 200, 000 pounds. ... At the Marshall Space Flight Center, we will soon dynamic test (fig. ... command service modules, lunar excursion module, and launch escape tower a all brought together for the first time foranbsp;...
|Title||:||Hearings, Reports and Prints of the Senate Committee on Aeronautical and Space Sciences|
|Author||:||United States. Congress. Senate. Committee on Aeronautical and Space Sciences|