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
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 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.
Speech to be delivered to Joint AIAA/ASME Student Chapters Meeting, University of Tennessee, Knoxville, Tennessee. Speech focusing on their future endeavors and missions into space.
As this paper is being written, the Saturn I flight test program includes five flights launched between October, 1961 and January, 1964. All five fiights were complete successes, both in achieving all major test missions and in obtaining an unprecedented volume of system performance data for flight analysis.
The Workshop project calls for changing a spent Saturn S-IVB propulsion stage into. living and working quarters after it has propelled itself into space.
The leaflet outlines the history of Saturn launches and gives a physical description of the rocket. The description includes a diagram of each stage; specifications of each stage's thrust, propellants, liftoff weight, and burning time; and engine specifications.
