Browse Items · UAH Archives, Special Collections, and Digital Initiatives

"Memorandum for Mr. Webb from George E. Mueller."

Memorandum discussing a review of the data of the Apollo 5 flight.

"Memorandum for Dr. Thomas O. Paine, Acting Director from George E. Mueller, Associate Administrator for Manned Space Flight, dated November 11, 1968."

Memorandum containing a recommendation from General Phillips to continue with the lunar orbit flight scheduled for December.

letfrogeoemueassadmformanspaflitomrjlatwprenorameaviinc_020408134617.pdf

Letter to Mr. J. L. Atwood.

Letter to J. L. Atwood from George M. Mueller regarding the S-II stage.

Address by Dr. George E. Mueller, Associate Administrator for Manned Space Flight, National Aeronautics and Space Administration before the Ninth National Conference of United Press International Editors and Publishers, October 8, 1968.

"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.

dynaenvioftheS-IVandS-IVBsatuvehi_062007110209.pdf

"Dynamic Environments of the S-IV and S-IVB Saturn Vehicles."

The vibration and acoustic environments of the S-IV and S-IVB Stages of the Saturn vehicle are summarized. A brief review of techniques used to predict the dynamic environments of the S-IV and S-IVB vehicles is presented. This review includes discussions on the prediction of rocket exhaust noise, boundary layer noise, sinusoidal vibrations, and random vibrations for the S-IV and S-IVB vehicles. In addition, sine-random vibration conversions are given.

"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.

"MSC/Apollo program management"

The purpose of this document is to describe how the Manned Spacecraft Center is managing its responsibilities in the Apollo Program The organization, procedures, and management philosophy described herein, represent the accumulated knowledge gained from our experience with the Mercury, Gemini, and Apollo Programs. It should be remembered, however, that managing a research and development program of Apollo's size and complexity, is an experimental "R&D" process in itself.

"Apollo 4 press kit."

The flrst flight test of the Apollo/Saturn V space vehicle is scheduled for launch from the Natlonal Aeronautics and Space Administration's John F, Kennedy Space Center, Fla., no earlier than Nov. 7. The mission is designated Apollo 4.

"Survey of Saturn stage test and checkout computer program development."

This survey of the Saturn Stage Test and Checkout Computer Program Development contains a summary description of the systems developed for factory and static test of the stages of the SATURN IB and SATURN V Vehicles. The responsibilities of the MSFC and stage contractor organizations that are involved in test and checkout computer program development are briefly described. The test and checkout hardware and software (computer program) systems are given for each stage and for each site where tests are conducted. The systems and procedures that are used for program production verification, documentation, and change control required for the implementation of planned computer programs are included. Notes are included in the report to indicate what material is missing or incomplete. No attempt has been made to draw any conclusions regarding the automatic test and checkout systems being developed for each stage and the manner in which the efforts are organized, scheduled, and implemented. This document has been based on material provided by stage contractors and by components of MSFC through May 1, 1966. COMPUTER SYSTEMS SECTION. VEHICLE SYSTEMS INTEGRATION BRANCH. VEHICLE SYSTEMS CHECKOUT DIVISION.; SR-QUAL-66-3.

The "Apollo/Saturn Guide for the Preparations of Specifications: Volume II of II Volumes."

This reproduced copy contains 43 pages of "general instructions for the uniform preparation of Project, System, and Contract End Items Specifications for Apollo/Saturn new equipment and major refurbishment."

"Proceedings : second NASA-wide reliability & quality assurance meeting : NASA Headquarters, November 29 - December 1, 1966."

The papers presented at the second NASA-Wide Reliability and Quality Assurance Meeting are published to disseminate current experiences and information. These papers, presented at NASA Headquarters on November 29 - December 1, 1966, are one means of exchanging current NASA reliability and quality assurance knowledge between projects and programs. This publication has been marked "FOR NASA USE" since it contains management opinions and contract experiences. Publication of papers suitable for wide dissemination in the Government, industry and University community is expected to be made separately. John E. Condon, Director, Reliability & Quality Assurance.

Apollo 8 Mission Operation Report.

This report is meant to provide NASA Senior Management with information on flight plans, mission objectives, and the basis for assessment of mission accomplishment. Note that page 61 is missing from the report.

"Apollo Documentation Administration Instruction."

According to the foreword found on page i, this document includes instructions on "procedures, methods and practices...necessary for the effective management of a program documentation system."

"Apollo 4 Pre-Launch Press Conference."

This document contains a transcription of the pre-launch press conference for Apollo 4. It includes the questions asked and answers given by participants Dr. Robert C. Seamans, Dr. George E. Mueller, Major General Samuel C. Phillips, Dr. Kurt H. Debus, and Dr. Wernher von Braun.

Technical information summary of the Apollo Saturn 1B flight vehicle.

According to the summary found on page 1, this document "presents a brief and concise description of the AS-204/LM-1 Apollo Saturn Space Vehicle." The information within the document allows readers to follow the timeline of the space vehicle's lift-off and journey to space.

"Apollo 5 Post-Launch Press Conference."

This document contains the transcription from the Apollo 5 post-launch press conference, including all the questions asked and answers given by participants Major General Samuel C. Phillips, Rocco A. Petrone, and Colonel William Teir.

"Apollo 5 Pre-Launch Press Conference."

This document contains a transcript of the pre-launch conference, including the questions asked and the answers given by participants William C. Schneider, Rocco A. Petrone, George M. Low, Col. William Teir, Col. Royce Olson, Christopher C. Kraft, Jr., and Eugene F. Kranz.

"Saturn display set: instruction manual."

The manual comprises a multi-volume set, the contents of which are as follows: VOLUME 1 -- a. Chapter 1 contains a general description of the equipment and its purpose, the physical and functional characteristics, and other pertinent data. b. Chapter 2 describes and illustrates the display set installation considerations. c. Chapter 3 lists and illustrates all operating controls and indicators. Chapter 3 also contains normal and emergency operating instructions.

"Saturn launch vehicles : security classification guide."

This security classification guide is a compilation of previous individual classification assignments. Consideration of international affairs, the use and development of advanced technological information, and requirements of flight safety have influenced these assignments.

"The U.S. manned space flight program: Mercury, Gemini, Apollo."

Exerpt from George E. Mueller giving a statement to Congress.

"Apollo/Saturn Guide for the Preparation of Specifications: Volume I of II Volumes."

According to the purpose found in section 1.1, "Volume I provides a guide for the preparation of specifications for existing equipment in the Apollo/Saturn Program."

"Press release : NASA starts development on ATM."

Press release describing NASA's plans to begin manned missions set to begin in 1968.

"Apollo 9 carries lunar module."

Press release surrounding the Apollo 9 rocket and its crew prior to launch.

"Research grants and contracts awarded to 25 : NASA news."

Press-release detailing 27 research grants sent to numerous universities.

qualassuprovforgoveagen_070207093109.pdf.pdf

"Quality assurance provisions for government agencies."

NASA Quality publication that contains requirements designed to facilitate the execution of programs effectively.

"Apollo Saturn LIEF Operations Plan."

This paper identifies the support functions performed by MSFC through the Launch Information Exchange Facility (LIEF) during the Apollo Saturn Mission Operations and other facilities required to carry out these functions. It also identifies mission specific documents required for operation. Note that page 20 is missing.

Bibliography of AEDC J-2 engine test reports.

Includes a letter to David L. Christensen, Research Institute, University of Alabama, Huntsville, Alabama from James Neely, dated March 18, 1969, with the subject line, "Technical paper entitled 'Start Transient Investigation of the Rocketdyne J-2 engine at Simulated Altitude Conditions.' " The bibliography of all AEDC J-2 engine test reports between July 1966 and Octoebr 1968 is attached.

LettMSFCAttnDrWernVonBraun_090408155515.pdf

"Project High Water."

Letter to Wernher von Braun from NASA headquarters regarding Project Highwater and how it was withheld.

"Pratt & Whitney Aircraft RL10 liquid hydrogen rocket engine"

Photograph of a Pratt & Whitney rocket engine.

"Saturn S-IV cryogenic weigh system. Part I : propellant utilization."

In order to achieve maximum vehicle efficiency, it is essential that the vehicle propellants be loaded to desired values and that these propellants approach simultaneous depletion at the end of powered flight. To accomplish precise loading and assure minimum residuals, a highly accurate and repeatable, vehicle located, propellant management (PM) or propellant utilization (PU) system must be used. As the ability to load propellants to predetermined values depends directly on the ability of the system to accurately sense the propellant masses, it is essential that the system be calibrated with respect to propellant mass under conditions resembling those to be experienced during final loading and powered flight. The use of a cryogenic weight system will reduce the unknown factors in capacitance sensor element shaping, tank geometry, and propellant properties to a degree which will permit the determination of propellant masses to with .025%.

"Manned planetary flyby missions (based on Saturn/Apollo Systems) : executive summary report."

This report summarizes a study (by North American Aviation, Space Division) of Manned Interplanetary Flyby Missions to Venus and Mars during the period from 1975 to 1982. [The study was a broad but penetrating technical investigation of using a manned flight system for planetary exploration.] The results, along with previously known aspects of manned Mars and Venus flyby missions, vehicles, and systems, were integrated into total mission-system capable of performing a realistic and meaningful planetary exploration program. Manned Planetary Missions are feasible. Attractive multiplanet flyby missions can be performed by Saturn/Apollo systems. However, injected payload and mission requirements developed within the guidelines and assumptions of this study cannot be met with modified S-II or S-IV stages when used with the standard Saturn V Earth-launch vehicle. When using an Earth orbit assembly mode and an uprated Saturn Earth launch vehicle for application to manned planetary flyby missions, the launch vehicle should have a payload capability (2-stage to low Earth orbit) of 400,000 pounds or more for use with M(S)-IVB planetary injection stages. Manned planetary flyby missions provide a means of combining the favorable aspects of both manned and unmanned missions into a unique and highly effective planetary exploration mission-system capable of providing major significant inputs to the scientific and engineering questions concerning the interplanetary medium, our Sun, and our neighboring planets Venus and Mars.

"Evolution of a Space Capability."

Two different organizational charts.

"Manufacturing plan for Saturn S-II, Stages 16-25."

Manufacturing plan for for SII stages 16 through 25.

"Organizational charts for Rocketdyne, a Division of North American Aviation, Inc."

Chart No. 1 Rocketdyne master approved by S. K. Hoffman, President (Vice President, North American Aviation, Inc.,).; Chart No. 6.1 Engineering Field Laboratories approved by R. J. Lodge, Director.; Chart No. 6.1.1 Santa Susana Field Laboratory, approved by D. M. Carpenter, Manager.; Chart No. 6.1.2 Field Laboratories Nevada Field Laboratory approved by G. J. Wunderlin, Manager.; Chart No. 6.1.3 Edwards Field Laboratory approved by F. F. Twight, Manager.; Chart No. 6.6 Engineering Administration approved by P. J. Kanne, manager.; Chart No. 12 Solid Rocket Division approved by T. E. Myers.

"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.

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