With respect to the SATURN IB launch vehicle, we have determined that it is practicable to provide 2, 000 pounds of ... To meet the SATLa#39;RN 1B requirements. the thrust 01a#39; the first stage engine. the Ha1, was increased from 188.000 to 200.000 pounds. ... At the Marshall Space Flight Center, we will soon dynamic test (fig. 57. p. 189) a complete flight-type APOLLO/SATURN IBa first and second stages, instrument unit, command service modules. lunar excursion module, and launchanbsp;...
|Title||:||NASA Authorization for Fiscal Year 1971|
|Author||:||United States. Congress. Senate. Committee on Aeronautical and Space Sciences|