This document is an official release of Manned Space Flight and its requirements shall be implemented by all cognizant elements of Manned Space Flight Program. William Teir, Manager, Saturn IB Program; E. F. O'Connor, Director, Industrial Operations; Wernher Von Braun, Director, Marshall Space Flight Center; Samuel C. Phillips, Director, Apollo Program.
The results of an OMSF AS-201 Interlock and RCA 110A Computer Review were published. Recognizing that this was a "quick look", it was determined that a more detailed approach should be taken with respect to interlocks for the duration of the Saturn IB-V program.
The manual comprises a multi-volume set, the contents of which are as follows: VOLUME 1 -- a. Chapter 1 contains a general description of the equipment and its purpose, the physical and functional characteristics, and other pertinent data. b. Chapter 2 describes and illustrates the display set installation considerations. c. Chapter 3 lists and illustrates all operating controls and indicators. Chapter 3 also contains normal and emergency operating instructions.
This handbook provides a technical data summary for the Douglas-produced Saturn S-IV and S-IVB stages of the NASA Apollo Program. Material contained in the S-IVB stage of this handbook includes the S-IB and S-V vehicles. This book will be updated as changes and additional information become available. The appendix contains aerospace fluid characteristics, LOX and LH2 vapor pressure curves and a list of non-standard abbreviations.
The Saturn C-1 space vehicle system is being developed by government agencies at industrial firms under the direction of the National Aeronotics and Space Division
Douglas Aircraft Company Report DAC-56445, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during August and September 1966. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-101.
This publication has been prepared to provide preliminary inspection requirements and limitations on all ground support equipment to support the Saturn II stage of the Saturn V launch vehicle.
