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. ... instrument unit, command service modules, lunar ex cursion module, and launch escape tower a all brought together foranbsp;...
|Title||:||NASA Authorization for Fiscal Year 1966, Hearings ...89th Congress, 1st Session, on S. 927|
|Author||:||United States. Congress. Senate. Aeronautical and Space Sciences|