S-IVB 200 Series

The 200 Series S-IVB


The S-IVb went through an evolutionary process before becoming the third stage of the Saturn V. As such, it was the first stage ready for flight testing. It started out as the second stage of the Saturn I, powered by six RL-10 liquid hydrogen engines. It was then enlarged, lengthened, and equipped with the J-2 engine for use on the Saturn Ib and Saturn V.

There were two distinct versions: A 200 series for use on the Saturn IB, and a 500 series for the Saturn V. The diagrams below explain the major differences, the most visible being the use of a larger Auxillary Propulsion System (APS) module on the 500 series. Also, the 200 series used three solid fuel ullage motors while the 500 series had two. The APS on the latter had a ullage function since the S-IVB was required to restart to send the Apollo Spacecraft to the moon.

"Ullage" is an old brewers term meaning the air space above beer in a vat. To restart the J-2 engine, the propellants must be at the "bottom" of the tanks, with the gas above them. If they aren't in this position, the fuel pumps would "cavitate" or suck up gas and the restart would fail.








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Copyright 1997, 1998 by John Duncan
Comments and questions welcome. All photographs contained on these pages are the author's, unless otherwise noted. No unauthorized reproduction without permission.

Last update: March 1, 1998