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Browse Items (1965 total)
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"Saturn and the Gulf Coast."
Presentation about the Saturn program and its purpose in the gulf coast. -
"Saturn history documentation: subject index."
This document explains the handwritten numbers on each document.; On spine is the title "Saturn history subject categories." -
"Saturn IB ESE interlock system."
The results of an OMSF AS-201 Interlock and RCA 110A Computer Review were published. Recognizing that this was a "quick look", it was determined that a more detailed approach should be taken with respect to interlocks for the duration of the Saturn IB-V program. -
Saturn IB launch project development plan.
This document is an official release of Manned Space Flight and its requirements shall be implemented by all cognizant elements of Manned Space Flight Program. William Teir, Manager, Saturn IB Program; E. F. O'Connor, Director, Industrial Operations; Wernher Von Braun, Director, Marshall Space Flight Center; Samuel C. Phillips, Director, Apollo Program. -
"Saturn IB news reference."
Images, decriptions, graphics and explanations of the various Saturn rockets. -
"Saturn IB - Saturn V instrument unit technical facts."
Press release detailing the technical aspects of the Saturn IB. -
"Saturn I engine gimbal and thrust vector control systems."
The hydraulic systems for the two-stage block II Saturn I vehicle are described with the evolution of their development. -
"Saturn I : the first generation of heavy launch vehicles designed for peaceful exploration of space."
A basic description of the Saturn rockets alongside diagrams for context. -
"Saturn I flight test evaluation."
Speech to be delivered to Joint AIAA/ASME Student Chapters Meeting, University of Tennessee, Knoxville, Tennessee. Speech focusing on their future endeavors and missions into space. -
"Saturn I/IB Launch Vehicle Operational Status and Experience."
6Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California. -
"Saturn illustrated chronology : April 1957 - August 1963."
A list of images with detailed descriptions of what they are and their histories. -
"Saturn instrumentation systems."
Paper to be presented at the Third International Flight Test Instrumentation Symposium College of Aeronautics. A brief description of the Saturn vehicles is given, delineating the makeup of and differences between the Saturn I, Saturn IB, and Saturn V. -
"Saturn I summary."
Summary of the history of the Saturn 1, its missions and its construction. -
"Saturn I workshop, 1968."
The Workshop project calls 'for changing a spent Saturn S-IVB propulsion stage into a living area after it has propelled itself into space. -
"Saturn I workshop, 1969."
The Workshop project calls for changing a spent Saturn S-IVB propulsion stage into. living and working quarters after it has propelled itself into space. -
"Saturn I/IB quarterly film report no. 25."
Memo gives dates and times of the interlock for final I.O. approval. -
"Security classification review of Saturn I/IB quarterly film report, no. 25."
Memo to Mr. Lee Cropp informing that the subject film report was reviewed for security classification. -
"Security classification review of Saturn I/IB quarterly film report, no. 25."
Memo to Mr. Lee Cropp, I-RM-D. -
"S-IVB Saturn high energy upper stage and its development."
The development of carrier rockets For manned space missions has been one of the major activities in the aerospace field during the past decade. The early space efforts were made possible by the existence of large ballistics missiles. It soon became obvious that the delivery of weapons and the launch of large spacecraft could not be combined into one operational system in an efficient way; therefore, a family of spacecraft boosters had to be created. -
"SAA program specification - case 218."
Memo sent to Major General D. M. Jones - NASA/ML. -
"Safety engineering for the man."
Presented at Safety Engineering of Missile/Space Systems, 53rd Air Force - Industry Conference, detailing potential safety issues within the Atlas weapon system. -
"Annual progress report :1966-1967."
The Annual Progress Report from July 1st, 1966 through June 30thm 1967. -
"Satellite recovery system."
Report focusing on the problems of the satalite recovery system and the possible solutions for those problems. -
"The Saturn IB launch vehicle system."
Speech containing information regarding Crystler's role in the Saturn Project as contracted builders of the stages of three space vehicles. -
"Saturn IB : presentation to Little Rock Group."
Speech by H.D. Lowrey, SAE Meeting, Detroit, Michigan. Focuses on the Apollo project, the technology involved and what the goals of the project are. -
"Saturn IB/V instrument unit."
This brochure provides some basic, general information about the lnstrument Unit, a very important part of the Saturn IB and Saturn V launch vehicles. These launch vehicles are being developed primarily for the Apollo program for manned lunar exploration but will also be used for future space missions. -
"Saturn I flight test evaluation."
As this paper is being written, the Saturn I flight test program includes five flights launched between October, 1961 and January, 1964. All five fiights were complete successes, both in achieving all major test missions and in obtaining an unprecedented volume of system performance data for flight analysis. -
"Saturn I/IB quarterly film report no. 26."
Memo is from Chief, Program Management Information, I-RM-D.; The date and time of the interlock for the final I.O. approval is given. -
"Saturn illustrated chronology : April 1957 - November 1962."
Document detailing the history of the saturn project between April, 1957 through November, 1962. -
"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. -
"Saturn S-IVB quarterly technical progress report."
Douglas Aircraft Company Report DAC-56533, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during January, February, and March 1967. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-01.; Prepared for National Aeronautics and Space Administration under NASA contract NAS7-101.; Approved by A. P. O'Neal, Director, Saturn Development Engineering. -
"Saturn S- II quality & reliability assurance : quality and reliability assurance" Organizational Chart.
Organizational Chart of the Rockwell Corperation, 1968 -
"Saturn S-IV cryogenic weigh system. Part IV : safety."
During cryogenic weigh system operation, hydrogen when combined with oxygen can create an unsafe condition. Therefore the concentration of the residual oxygen and hydrogen from leaks in the cryogenic weigh environmental bags must be known at all times during the cryogenic weigh. Hydrogen and oxygen detectors will provide the optimum method for maintaining safe conditions. Hydrogen properties and safe mixtures are reviewed. The method selected to analyze the oxygen content is discussed. The selection, development, and testing of a hydrogen detector system is examined. -
"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%. -
"Saturn S-IV cryogenic weigh system. Part II : weigh operations."
Two basic methods for mass determination are: (1) direct measurement, (2) volume and density determination. Both methods or variations have been used to determine space vehicle propellant mass with varying degrees of success. Stringent propellant loading accuracy requirements of k0.5 percent for the Saturn S-IV Stage have led to the development of a Cryogenic Calibration Weigh System. The method employs accurate electronic force transducers and measuring systems as the standard and experimental weighings have verified achievement of better than the required accuracy. -
"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. -
"Saturn IB/V Instrument Unit system description and component data: technical manual."
This manual contains a brief description of each Instrument Unit (IU) system and their respective components for S-IU-201 through 212 and S-IU-501 through 515. -
"Saturn and its mission."
Presentation from Harper, discussing the Saturn Project's then-status, background and plans. -
"Saturn and the exploration of space."
Presentation Raymond Pisani to the East-West Bank Chamber of Commerce regarding the Saturn project's roll in space exploration and what contrabutions the East-West Bank can make in that area. -
"Saturn and the future."
Presentation with its main focus on the competitive and humanitarian goals of the Saturn project.