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"Manufacturing plan for Saturn S-II, Stages 16-25."
Manufacturing plan for for SII stages 16 through 25. -
"Saturn S-II stage program plan."
This documents outlines the S & ID plan to fulfill the requirements of Contracts NAS7-80 and NAS7-200 for the design, development and manufacture of the Saturn S-II stage.; APPROVED by R E. Greer, Vice President and S-II Program Manager.; This reissue supersedes all previous issues of this report.; FOREWORD: The S-II stage is 81.5 feet in length and 33 feet in diameter, with a usable propellant capacity of 970,000 pounds, The S-II propellants are fully cryogenic-liquid oxygen at -279 F and liquid hydrogen at -423 F. Its five-engine cluster provides one million pounds of thrust. The stage is a cylindrical structure of relatively light weight with a shell designed to resist all loads without the use of stiffening members. Its skin is of welded aluminum panels, as are the elliptical bulkheads of the fuel and oxidizer tanks. Unique to its design is the common bulkhead that separates the -423 F liquid hydrogen from the -247 F liquid oxygen. The common bulkhead - a sandwich of two 33-foot diameter aluminum domes separated by an insulating filler of honeycomb - eliminates the weight penalty that would be imposed by the second bulkhead in more conventional design. This document describes the S & ID program plan for development of the S-II stage and associated a support equipment. -
"Saturn S-II annual progress report 1 July 1963 through 30 June 1964."
This document is the second annual progress report of the Saturn S-II Program. The report provides a summary and technical analysis of results of contract work by the Space and Information Systems Division of North American Aviation, Inc., for the period 1 July 1963 through 30 June 1964. This document was prepared in compliance with NASA contract NAS7-200. -
"Saturn S-II : annual progress report : 1 July 1962 through 30 June 1963."
This document, prepared in compliance with NASA contract NAS7-200, is the first annual progress report on the Saturn S-11 Program at the Space and Information Systems Division of North American Aviation, Inc. It provides a summary- and a technical analysis of results of contract work for the period 1 July 1962 through 30 June 1963.; SID 63-1028-1 251 pages. Include illustrations. -
"The Common Bulkhead for the Saturn S-II Vehicle: Unique Manufacturing Effort Adds to Space-Age Hardware Technology".
Presentation regarding the construction of Apollo and Saturn rockets. -
"Documentation List for Saturn Stages S-11."
The information presented in this document represents a listing of all formal documentation prepared under contract NAS7-200. The listing has been arranged under major categories as specific in SID 61-366A, reissued 10 August 1964. Within each categorization , the reports and specifications have been listed in numerical sequence. -
"Engineering : Saturn S-II program"
Organizational chart diagram of the North American Rockwell Corporation Engineering division: 10-14-1968 -
"Inspection of Welds on S-II-1."
Archive copy is a poor photocopy. Cannot read. -
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"Material : Saturn S-II program."
Saturn S-II Program Organizational chart.