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"Design Concepts of Ground DDAS in Saturn 1B/V ESE."
In the Saturn IB/V programs the sheer quantity of data required for computer processing and ESE display makes it necessary to provide an efficient data acquisition system. For much of the data originating in the launcher this requirement is satisfied by the Ground Digital Data Acquisition System (DDAS). This paper provides a technical description of the Ground DDAS with emphasis placed on the unique design concepts of this telemetry system. -
"Application of the Saturn V Launch Vehicle to Unmanned Scientific Exploration of the Solar System."
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." -
"Assessment of Risk for Engineering Change Decisions."
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." -
Differences of configuration in successive Saturn IB and Saturn V vehicles- case 330.
Includes memorandum for file. Configuration matrices reflecting present program status of differences in Saturn IB and Saturn V flight hardware on a mission to mission basis have been prepared. The attached matrices are arranged to show differences in major subsystems (Structures, Propulsion, Instrumentation and Range Safety, and Electrical) for each stage. The reason for the configuration difference and the mission effectivity are included.; DMD, 2031-SGE-eas, GRH; Includes "Recommendation for announcement and distribution of Bellcomm Report".