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"Instrument Unit Program Review : Saturn Instrument Unit."
Handwritten names and phone numbers on the first page. Apollo / Saturn Team. -
"NASA management programs."
Address by Dr. George E. Mueller, Associate Administrator for Manned Space Flight, National Aeronautics and Space Administration; Joint AIAA/CASI Meeting, Montreal, Canada, July 8, 1968. AS DELIVERED.; Includes charts. -
"Propulsion and Vehicle Engineering Laboratory monthly progress report (April 1, 1966 through April 30, 1966)."
Progress report for the month of April, 1966. -
"Propulsion and Vehicle Engineering Laboratory monthly progress report (March 1, 1966 through March 31,1966)."
A collection of progress reports covering a large number of projects within the month of March, 1966 -
"Propulsion and Vehicle Engineering Laboratory monthly progress report (November 1, 1966 through November 30, 1966)."
A collection of progress reports covering a large number of projects within the month of November, 1966 -
"Propulsion and Vehicle Engineering Laboratory monthly progress report (August 1, 1966 through August 31, 1966)."
A collection of progress reports covering a large number of projects within the month of August, 1966 -
"Propulsion and Vehicle Engineering Laboratory monthly progress report (July 1, 1966 through July 31,1966)."
A collection of progress reports covering a large number of projects within the month of July, 1966 -
"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 V project development plan : November 1967.
This document revises and supersedes the Saturn V Project Development Plan, dated March, 1967. Approved: Arthur Rudolph, Manager, Saturn V Program; Samuel C. Phillips, Major General, USAF, Director, Apollo Program.