
Image Credit: NASA
Image source: Mike Acs

Image Credit: NASA
Image source: Mike Acs

Image credit: Douglas
Image source: Mike Acs

Image credit: McDonnell Douglas
Image source: SDASM Archives

Image credit: McDonnell Douglas
Image source: Drew Granston


Image credit: North American Rockwell
Image source: Numbers Station

Image credit: North American Rockwell
Image source: Numbers Station

This undated cutaway drawing illustrates the Saturn IB launch vehicle with its two booster stages, the S-IB and S-IVB. Developed by the Marshall Space Flight Center (MSFC) as an interim vehicle in MSFC’s “building block” approach to the Saturn rocket development, the Saturn IB utilized Saturn I technology to further develop and refine the larger boosters and the Apollo spacecraft capabilities required for the marned lunar missions.
Image credit: NASA MSFC
Image source: NASA Images

Conceptual view of the operations in the equatorial earth orbit. The operation in orbit is principally one of propellant transfer and it not an assembly job. The vehicle being fueled is the third stage of a SATURN II with a lunar landing and return vehicle attached. The third stage of the SATURN II was used in the combination into orbit and has thus expended its propellants. This stage is fueled into orbit by a detachment of approximately ten men after which the vehicle then proceeds on the moon.
Image credit: United States Army
Image source: NASM

Image credit: Ryan Aeronautical
Image source: SDASM Archives




Eagle Book of Rockets and Space
by John W.R. Taylor and Maurice Allward
Longacre Press, 1961
Image credit: NASA
Image source: Numbers Station