Browse Items (27 total)
Sort by:
-
"The toughest weld of all" S-II stage manufacturing.
Article explores the outer layer of the Saturn S-II along side its benefits and complications. Contains poorly rendered images displaying the process. -
"Telegraphic message : inspection requirements for S-II-1 and S-II-2 at KSC."
Photocopy of an inspection list requirements for S-II-1 and S-II-2. -
"Test operations:" Organization Chart.
Organization Chart of the North American Rockwell Test Operations. -
"S-II Engine."
8 x 10 inch black and white diagram of the Saturn II engines. -
"Saturn S-II facilities organization."
Organizational chart for the Saturn II facilities. -
"The Saturn S-II."
The S-II is the second stage of NASA's Apollo moon-landing rocket - the giant Saturn V. The most powerful hydrogen-fueled booster under production, the S-II is destined for Apollo manned lunar missions and will help power three Americans to the moon. The S-II is being developed and manufactured at Seal Beach, Calif., by North American's Space and Information Systems Division, Downey, Calif., under the technical direction of NASA's Marshall Space Flight Center, Huntsville, Ala. -
"Saturn S-II general manual."
This manual contains information covering the second stage of the Saturn V launch vehicle. -
"Saturn S-II ground support equipment inspection manual."
This publication has been prepared to provide preliminary inspection requirements and limitations on all ground support equipment to support the Saturn II stage of the Saturn V launch vehicle. -
"Saturn S- II quality & reliability assurance : quality and reliability assurance" Organizational Chart.
Organizational Chart of the Rockwell Corperation, 1968 -
"Saturn stages S-II : July 7, 1961 : Minutes of the phase II pre-proposal conference for stage S-II procurement."
Transcription of a confrence aiming to propose ideas for new rocket designs. Includes references to slides. -
"Response to any news media queries concerning MSFC S-II stage."
Letter to answer any incoming questions from the media regarding the MSFC-II stage and any briefed on Seal Beach. -
Program Planning and Control : Saturn S-II program Organizational Chart."
Saturn S-II Program organizational chart of 1968. -
"Memorandum : S-II Stage Program Report from MA/Apollo Program Director to MA/Associate Administrator for Manned Space Flight."
Includes enclosure of S-II Stages Status.; Archive copy is a poor photocopy. -
"Manufacturing plan for Saturn S-II, Stages 16-25."
Manufacturing plan for the Saturn S-II." -
"Manufacturing Organizational Chart : Saturn S-II program."
Organizational chart of the North American Rockwell Corperation : 1968. -
"Material : Saturn S-II program."
Saturn S-II Program Organizational chart. -
"Inspection of Welds on S-II-1."
Archive copy is a poor photocopy. Cannot read. -
"Engineering : Saturn S-II program"
Organizational chart diagram of the North American Rockwell Corporation Engineering division: 10-14-1968 -
"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. -
"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. -
"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. -
"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 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. -
"Manufacturing plan for Saturn S-II, Stages 16-25."
Manufacturing plan for for SII stages 16 through 25.