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"Memorandum, routing slip, and letter by Harold G. Russell, Colonel, USAF, concerning the Business Week article 'North American tries to advance under fire.'"

This document also contains part of the Business Week article "North American tries to advance under fire", (June 3, 1967) pages 154 to 162. The complete article can be found at the UAH Library in microfilm format.; The document has handwritten notes and is a poor photocopy.

theuseofwindsheainthedesiofaerovehi_103107103412.pdf

"The use of wind shears in the design of aerospace vehicles."

Prepared for presentation at the 23rd Meeting of the Structures and Materials Panel, AGARD, October 4-11,1966, ONERA, Paris, France.; ABSTRACT: The relative influence of various wind profile properties and disturbances on launch vehicle flight dynamic response is studied. Particular emphasis is placed on the influence of wind shears and turbulence on dynamic response during the boost phase of the flight. Four hundred and seven individual detailed (Jimsphere) wind profiles are the primary wind inputs for this analysis. Time response of the vehicle to each profile is computed and a statistical evaluation of the results made. Results are obtained for the Saturn V space vehicle and conclusions drawn as to the relative influence of wind shears and turbulence vs the degree of refinement of the dynamic model of the space vehicle.

"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."

This paper includes the equations for the bending moment of a launch vehicle with the effects of bending and sloshing dynamics. It also includes a comparison between the bending moment response envelope of the measure winds and the bending moment response of the MSFC synthetic wind profile.

dynloaofalauvehduetoinfwin_121307141031.pdf

"Dynamic Loads of a Launch Vehicle Due to Inflight Winds."

Analysis of the stability and dynamic load environment of a launch vehicle resulting from atmospheric disturbances is a very complex problem. To determine the dynamic load environment of the vehicle requires an adequate description of the wind field, vehicle dynamics and control system. The essential of such a study, namely methods of analysis, wind field specification and representative vehicle response parameters for evaluation, are of equal importance. This paper is concerned with the mathematical foundations of the vehicle model and method of analysis.

Technical information Summary Apollo-11 (AS-506) Apollo Saturn V Space Vehicle.

The document's mission summary states "This documet is perpared jointly by the Marshall Sapce Fligh Center Laboratories S&E-ASTR-S, S&E-AERO-P, and S&E-ASTN-ESD. The document presents a brief and concise description of the AS-506 Apollo Saturn Space Vehicle and the AS-506 mission. Where necessary, for clarification, additional related information has been included. It is not intended that this document completely define the Space Vehicle, its sytems or subsystems in detail. The information presented herein by text and sketches, describe launch preparation, ground support activities, and the space vehicle. This information permits the reader to follow the sequence of events beginning a few hours before liftoff to mission completion."

drafinfoworkpaptechhistsaturn_031607103330.pdf

"Technical History of Saturn."

Draft of working paper. Typed with handwritten notes (title and author) and pages. Copy in MSFC files noted on first page.

Letter from Arthur E. Sanderson at Marshall Space Flight Center to Berta Mrazek in Huntsville, Alabama.

In the letter, Sanderson authorizes Mrazek to travel to Houston, Texas and Los Angeles, California "to participate in activities in connection with the Apollo 11 mission, at the invitation of the President of the United States."

"Application of Saturn Systems to Orbit Launch Operations."

Presented at the AIAA/AAS Stepping Stones to Mars Meeting, this paper compares the "payload velocity spectrum for existing and future missions" with Saturn V capabilities.

"Systems applications in orbital launch operations."

The objective is to examine the technical requirements and feasibility of conducting orbital launch operations with systems now in the development phase. In order to maintain realistic constraints on the analysis, the Saturn S-IVB stage has been used as an example of present stage technology. The requirements, procedures and complexity of operations for orbital assembly and launch are discussed. The primary design requirement for orbital assembly and launch operations is increased orbital stay time (from hours to days or weeks).

Letter to Robert K. Bell from Richard W. Satterthwaite.

Satterthwaite writes to Bell to aid him in the Nickerson case by providing suggestions for testimony and information regarding the information regarding the missile program, including its financial situation and impact if switched from the Army to the Air Force.

Saturn AS-501 evaluation bulletin No. 1, November 14, 1967.

The findings herein are the results of the combined evaluation efforts of the various Laboratories of Research and Development Operations at MFSC, The Boeing Company, North American Rockwell/Space Division, Douglas Aircraft Company, International Business Machines, and Rocketdyne.

"Report to the administrator, NASA on the Saturn development plan."

In anticipation of this transfer, the NASA and Department of Defense have established, an interim working agreement that provides for immediate assumption by NASA of responsibilities fortechnical management of the Saturn vehicle development.

"Monte Sano State Park."

"A spectacular view from Monte Sano State Park near Huntsville, Alabama. Color by Wayne Floyd."

"Apollo Logistic Support Systems."

According to an abstract found on the page following the title page, this paper includes "one possible conceptual definition of an early Apollo Logistics Support Systems (ALSS) is presented and various payloads for the system are briefly discussed. " It also discusses the Lunar Mobile Laboratory (MOLAB) and other considerations for a lunar scientific mission.

"Letter to Mr. Kurt R. Stehling."

Letter to Kurt R. Stehling from Julian Scheer answering on behalf of "Mr. Webb," stating that Kurt's "idea" was interesting and is to be given careful consideration.

"Memorandum to Dr. Emme - EH through Mr. Shafter - G from Julian Scheer, Assistant Administrator for Public Affairs, National Aeronautics and Space Administration."

This attached correspondence indicates a great deal of confusion and that a number of people are in the act. The matter before the house is whether we will (Dr. von Braun is asked) to allow Logsdon to have a copy of the Von Braun memo to the Vice President on space goals.

Survey of Automatic Checkout Systems for Saturn V Stages.

The Abstract states "The four checkout systems developed and utilized by the National Aeronautics and Space Administration (NASA) for acceptance checkout of the Saturn V launch vehicle stages and instrument unit are described. The vehicle's characteristics, test policies, equipment design criteria, and operational factors are reviewed. Following a general description of each checkout system, this paper presents a brief definitive description of each major subsystem test station. These test systems are used for post-manufacturing and post-static firing acceptance checkout. The section related to the S-II stage includes several representative flow diagrams and descriptions of automatic tests. To present in detail the large volume of information describing these four checkout systems would require the writing of four papers."

Letter to Robert K. Bell and Ray H. Jenkins from Major General Robert A. Schow, Assistant Chief of Staff, Intelligence.

Schow writes this letter in response to Bell and Jenkins request for classified information. Schow states that the convening authority will determine the relevance of the material before allowing access.

staproforusiuniofmasweiforpresandacc_031207095943.pdf

"Standard procedure for using units of mass, weight, force, pressure and acceleration."

Report No. DT-TM-1-60. ; FORWARD: The field of missiles and rockets deals with quantities of matter at various locations with different accelerations of gravity. The weight of these masses changes with gravity and the measurements of liftoff weight, fuel weight, etc., result in different values, depending on whether mass or weight units are used. Pressure and thrust are independent of the acceleration of gravity, but the instruments for measuring these values are calibrated with standard masses, producing different weight forces and calibration curves at different locations. Most sections of ABMA and other agencies or companies use pounds or kilograms as units of mass, weight or force, and the influences of different accelerations of gravity are often disregarded or treated incorrectly. These discrepancies become increasingly unacceptable with larger missiles and greater distances between operation sites. Therefore, the following Standard Procedure has been prepared to insure consistent and uniform terms and units of mass, weight, force, pressure and acceleration. All sections and individuals concerned are urged to use these units andprocedures. This is signed by Dr. Wernher von Braun, Director Development Operations Division.

"The role of weighing in the development and firing of missile and spaceships."

Speech regarding the importance of developing and upgrading space ships and space technology.

"Automatic Pressure Transducer Calibration System."

The abstract notes, "The development of an automatic pressure transducer calibration system is discussed in this report. Evolution from past practices and systems into an automatic calibration system with computerized data handling is described."

"Digital Transducers."

This paper outlines the major advantages of digital transducers and describes the principles and features (1) direct digital transducers, (2) indirect digital transducers, (3) quasi-digital transducers, and (4) A to D transducers.

"Lunar Applications of a Spent S-IVB/IU stage (LASS)."

Support of lunar exploration missions is a major consideration in future space program planning. The spent Saturn v/S-IVB/IU can support both lunar - orbit and lunar -landing operations. This paper investigates lunar applications of the spent stage, and incorporates data generated during Company-funded studies. Investigated here is the feasibility of using a launch vehicle employing standard S-IC and S-I1 boost stages to deliver a modified S-IVB/IU and large discretionary payloads to a lunar orbit (LASSO) and/or the lunar surface (LASS). Operations in Earth orbit and direct-ascent trajectories are examined, and consideration is given to the use of the spent stage as a shelter in a manner similar to the presently planned Earth orbital workshop operations. Both the LASSO and LASS concepts are recommended for consideration in future lunar exploration plans. These concepts are capable of placing a gross wet weight of 101,400 lb in lunar orbit or landing 63,580 lb on the lunar surface respectively. The effective payload capability can be enhanced by proper integration of translunar mission subsystems with the subsystems required for lunar orbit or surface operations. The vehicles can be available within 3 years, with current-technology hardware sufficient for performing the missions described.; Douglas Paper No. 4256.

Autobiography and résumé of William August Schulze.

In this partial autobiography, Schulze describes his experiences growing up in Neulaubusch, Germany and training and working as an engineer. He notes that he began working for Wernher von Braun at Kummersdorf in 1936 and then moved to Peenemünde, where he worked on the A-3, A-5, A-7, and V-3 rockets. The documents also include a lengthy handwritten excerpt from Schulze's 1945 day book and a résumé. Includes a transcription and a partial English translation.

Letter from August Schulze in Aberdeen, Maryland to Trude and Erika Schulze in Landshut, Bavaria, Germany.

Schulze wrote this letter to his wife, Trude, and daughter, Erika, on the back of a photostat copy of his War Department Notification of Personnel Action. In the letter, he discusses his pay and accommodations with the U. S. Army.

1946 day book.

Written by William A. Schulze, this day book includes notes from his activities at Army Proving Ground at Aberdeen, Maryland in early 1946. Schulze was transported from Germany to Aberdeen in late 1945 as part of the first group of German engineers sent to the United States. During the week of March 17-23, Schulze records his travel from Aberdeen to El Paso, Texas, leaving on Monday, March 18, and arriving in Texas on Thursday, March 21. The day book includes entries on shopping, leisure activities, birthdays, and mail. Schulze's notes reference H. N. Toftoy, Konrad Dannenberg, Wilhelm Jungert, Hannes Luehrsen, Theo Poppel, Erich Neubert, Walter Schwidetski, and others.

German state health insurance book and cards belonging to William August Schulze.

This booklet, "Sammelbuch der Bescheinigung über die Endzahlen aus der Aufrechnung der Versicherungskarten für August Schulze," documents Schulze's government health insurance while he was employed in Germany from 1930 through 1944. Each page serves as an insurance card for each year of employment. Page seven marks Schulze's first insurance record as an employee at Peenemünde.

Correspondence between William A. Schulze in Huntsville, Alabama, and Walter Dornberger in Buffalo, New York.

In his letter to Dornberger, Schulze congratulates him on his seventieth birthday and notes, "Looking back 29 years ago when I joined your organization in Kummersdorf, it is hard to single out specific important decisions you made and accomplishments achieved; to me they all appear of outstanding nature. I shall always be grateful for the friendship and experience gained in the development of rockets as a member of your team in those early years." Dornberger's reply is enclosed.

Excerpt from the 1946 daybook of William A. Schulze.

This excerpt includes pages 36 and 37 of the daybook. In the entries, Schulze notes his travel to Fort Bliss, Texas from Aberdeen, Maryland. A translation is included.

Statements by Charley Scott to the University of Alabama in Huntsville community.

This document is a text version of the statements Charley Scott made on May 16, 1964 on the education needs and challenges in Alabama. Scott notes that he is addressing "students, prospective students, parents, secondary school representatives, and members of the University of Alabama staff in Huntsville." He frequently quotes Dr. Frank A. Rose, President of the University of Alabama.

Letter from Charley Scott, Director of Instruction, to Christel McCanless, Librarian, at the University of Alabama Huntsville Center.

Scott notes his appreciation for McCanless' adept handling of the "Review of the Development of the Huntsville Campus Library."

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