Presented at the AIAA/AAS Stepping Stones to Mars Meeting, this paper compares the "payload velocity spectrum for existing and future missions" with Saturn V capabilities.
According to the foreword, "This paper presents the results of a twelve-week mission and systems analysis of a combined Jupiter orbiter/solar probe mission utilizing the Saturn V launch vehicle."
This paper focuses on an approach for achieving high reliability within the Navigation, Guidance, and Control systems of the Saturn class launch vehicles.
This paper, which was presented at a Semi-Annual Meeting of the American Rocket Society, traces the role of the United States Army in national space activities. Incorporated in the report are photographs illustrating the evolution of the satellite and space program.
"This report outlines, through a series of sketches with accompanying text, the general features of the SA-203 Launch Vehicle and information on launch preparation, the launch facility and mission peculiar experiments."
This document includes the current basis for approval of ECPs, fatigue life after stress reduction, and other probability and comparative risk assessments. On the first page there is an inscription, "By E.L. Bombara NASA-MSFC."
Prepared by A. W. Dryden, Quality Engineer, Quality Engineering, Reliability Assurance, Space Systems Center, Douglas Aircraft Company, Inc., Huntington Beach, California. Presented to the 21st Annual Technical Conference for the American Society for Quality Control, Chicago, Illinois. 30 May to 2 June 1967.
