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Correspondence between G. H. Milliken and Oscar Goldsmith about the Treasurership of Dallas Mnfg. Co.
These letters discuss the appointment of a new treasurer of Dallas Mnfg. Co. to succeed Mr. Rison. Oscar Goldsmith offers himself as an applicant for the position in the first letter. The second letter is Milliken's response to the topic. He states that Mr. Rhett has been selected for some time now while Mr. Rison was still there. Milliken thanks Goldsmith for his willingness to take on more work and hopes he will continue as Assistant Treasurer as he deems it "unwise for a man of your age" to take on additional responsibilities. Goldsmith replies in the final letter expressing happiness at Mr. Rhett's appointment and mentions the already-scheduled Director's Meeting. -
Correspondence between G. H. Milliken and Oscar Goldsmith about a visit to the mill in Huntsville from Milliken and Mr. Winchester.
Milliken writes to Oscar Goldsmith in the first letter stating that he hopes to visit the Huntsville mill with Mr. Winchester soon. Goldsmith responds that he would be glad to have them visit. -
Correspondence between G. H. Milliken, W. E. Winchester, and Oscar Goldsmith.
Correspondence between G. H. Milliken, W. E. Winchester, and Oscar Goldsmith regarding flowers bought for the funeral of Mr. Rison. -
Letter to K. Ward-Smith from Oscar Goldsmith.
A letter from Oscar Goldsmith to K. Ward-Smith regarding capital stock of the Dallas Mfg. Co. -
Correspondence between Hotchkin and Co. and Oscar Goldsmith.
The letters detail information about Dallas Manufacturing Co. stocks being sold. This set of documents also includes a check for the forty shares. -
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"Engineering Safety Into Missile-Space Systems."
Safety Engineering, as applied to complex missile and space systems, has developed a new methodology referred to as "System Safety Engineering." The requirement for a comprehensive approach to safety which is included as a contractually covered adjunct to the design, development, and operational phases of a systems life cycle has become apparent from costly missile mishap experience. The general concepts and accomplishments of this new engineering discipline are described along with possible beneficial relationships with Reliability and other recognized organizational elements engaged in safety related activities. -
"Uses of Saturn."
Saturn and Apollo hardware will not have realized their ultimate potential for space exploration after the project lunar landing is complete. To accomplish the Apollo lunar landing program, an immense backlog of technology, facilities, and booster capability will have been built up, and we believe proper utilization of this resource will fill the needs for planetary, lunar and earth orbital space exploration for years to come. -
"A survey of propulsion problems as related to space vehicle design."
Incomplete document. Displays errors in space-vehicle design as they relate to space travel. -
"Opportunities for European Payloads on the Saturn Vehicle."
Prepared for presentation to the Eurospace Conference. In this paper, we will not deal with the first two questions, which must be of interest to every potential experimenter, but only with the last question of vehicle availability. -
"High Energy Missions for Saturn."
Presented to Society of Automotive Engineers, Advanced Launch Vehicle & Propulsion Systems. When the Apollo lunar landing project is complete, the Saturn and Apollo hardware will only have begun to realize their ultimate potential for space exploration. The immense reserve of Apollo technology, facilities, and booster capability can then be directed to the achievement of national goals which lie far beyond the initial lunar landing. In achieving the Apollo lunar objectives, large investments will have been made in launch facilities, tracking systems, propulsion techniques, reentry systems, lunar landing systems and rendezvous technologies. Although developnent in these specialized areas has been tailored to the needs of Apollo, numerous studies by NASA and industry have demonstrated the feasibility of using the spacecraft, launch vehicles, and operating techniques for missions far more complex than lunar landings. Amortization of this hardware will prove cost-effective for missions of more sophisticated applications. -
"Evolutionary Steps in S-IVB Development."
The injection stage of a multistage launch vehicle must be partially a velocity stage and partially a spacecraft; it must not only boost the payload, it must also perform cooperative mission operations with the payload after orbital insertion. These hybrid requirements result in intrinsic stage versatility which permits consideration of new and challenging missions for the stage which were unanticipated during initial design.; Prepared by T. J. Gordon, Director, Advance Space Stations and Planetary Systems, Space Systems Center, Douglas Aircraft Company, Huntington Beach, California. -
"Minimax control of large launch boosters."
Keith D. Graham is principal mathematician, Systems and Research Center, Honeywell, Inc., 2345 Walnut Street, St. Paul, Minnesota.; Work done under NASA contract NAS 8-11206 from the George C. Marshall Space Flight Center.; ABSTRACT: A method of specifying the gains of a linear controller for a large launch booster using a new application of optimal control theory is described in this paper. Results for a specific example are included. An important control requirement is to maintain cost variables (such as bending moment, engine gimbal deflection, and lateral deviation from desired trajectory) within specified limits in the presence of load disturbances. This requirement is met by using a performance index which depends explicitly on maximum achievable values of the cost variables in a finite time interval. -
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"Payload integration for space experimentation."
Space experimentation requires an increasingly complex planning and systems engineering effort to meet the demand for highest precision and reliability of all measurements and observations. A companion paper discusses the interfaces between the scientific/technical areas of space experimentation and the instruments, subsystems and support systems within the spacecraft. This paper deals with the organization and the procedures which are needed to perform the difficult payload integration process for space experimentation. In the course of this process it is necessary to define the experiments completely, to describe all instruments in terms of engineering specifications, to investigate the commonality of equipment, to group the experiments into mission compatible payloads, to specify acceptable loads on all subsystems and astronauts (when present) and to plan for all contingencies during the flight. -
Technical Reports" Bibliography.
Bibliography of technical reports from 1957-1963 -
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Oral History Interview With Bran Griffin
Bran Griffin was born in Medford, Oregon. His father was in the military, so they moved around a lot. Bran went to the University of Texas his first year of college, and he studied Architecture. Then, he graduated college with a degree in Architecture from Washington State University. He then went to graduate scholl in Southern California, and he received a fine arts degree. After this, Bran wanted to get a degree in something a little more stable, so he went back to school to get his master's degree in Architecture. After this, Bran was on a shuttleship for a couple of years in Rome, and then he came back to start his career in teaching Architecture. Even though he was teaching Architecture, he had an intense passion for space. Because of this passion, he started to become involved with the Johnson Space Center with a faculty fellowship. Bran was in their Spacecraft Design Division. Since he wanted to be closer to be a part of the Space Industry, he decided to move to Washington State. After a while of working in Washington State, he received a job offer from Boeing in Hunstville, AL and began his career there being involved with the space station.Tags Oral History -
"Philosophy and practices of reliability as applied in the design of the Saturn Instrumentation System."
The basic engineering approach used in the Saturn instrumentation system has evolved to provide a highly reliable design for short periods of operation. The airborne measuring and telemetry systems including preflight tests, inspection, documentation, and feedback between the users and designers are discussed. The apparent differences between the practice and theory of reliability are rationalized. Some consideration is given to new problems in designing systems that must operate in hostile environments for long periods. The potential contribution of redundancy as a design concept is discussed.; This paper is concerned with the airborne measuring and telemetry systems; it does not attempt to treat the entire Saturn instrumentation system which consists of tracking devices including optical, radar, and Doppler, plus television, film cameras, and a myriad of instruments connected with factory checkout, ground test, and launch. -
Fee report for a claim suit filed by Lawrence Goldsmith against H. Oliver with Parks & Cotton.
This document contains a detailed breakdown of the fees associated with the "unlawful detainer suit" filed by Lawrence Goldsmith against H. Oliver. -
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"Liquid Rocket Engines."
This paper presents a discussion on liquid propellant rocket engines. The first part contains a discussion on liquid propellants, including a description of various propellant types such as cryogenic, storable,bipropellant, and monopropellant. This part also points out desirable physical properties and includes a section on performance outlining the methods by which performance is calculated and shows performance for various liquid rocket propellant combinations. -
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Personal letter to "Papa Oscar" from grandson Oscar.
This personal letter to Oscar Goldsmith from his grandson, also named Oscar, details the removal of young Oscar's tonsils and his gaining eight and a half pounds. He also writes of his first refrigerator sale and his hopes to sell more, though he is "no salesman". He conveys some information from his mom and thanks him for making her trip to New York possible. Finally, young Oscar thanks Papa Oscar for paying his tonsil removal bill, and promises that he can take care of his dentist bill. -
"The NASA/Grumman Apollo lunar module"
Handwritten in pencil on the document. Describes the layout and function of various sections of the Apollo lunar module. -
"Structure of the NASA/Grumman lunar module."
Describes the structure and function of each part of the NASA Lunar Module -
"Manufacturing history - LM-5."
Essay that focuses on the achievements of the Grumman Aerospace Corporation. -
"LM System Description."
Report that describes the major systems of the Lunar Module. -
"Development of the NASA/Grumman Lunar Module."
Paper regarding the actions and achievement of the Grumman Aerospace Corporation. -
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"Nuclear engine design considerations."
The intent of this paper is to examine the static test countdown organization and discuss the need for a systematic method to organize a countdown. -
Receipt of payment from E. H. S.
Receipt of payment of $8.50 from E. H. S. signed by Walter Gurley. -
More About the Cuca Cup
This is an article about the Cuca Cocoa Challenge Cup over 40 years after the event took place and specifically discusses the second cup and the challenges that led the demise of the Cuca Cocoa Challenge series. -
"Guidance and Control of Saturn Launch Vehicles."
The navigation, guidance, and control modes and problems of the Saturn launch vehicles are given as the requirements for the guidance and control methods. Two path adaptive guidance modes, featuring flight path optimization, in the form of a polynomial mode and an iterative mode are given in their computation form and compared with respect to mission flexibility, implementation requirements, and performance. Attitude control during the propelled flight phases requires consideration of various bending and sloshing modes; stability of the control system is obtained by phase stabilization of the low frequencies and by attenuation of the higher frequencies. Typical shaping networks and their transfer functions are given. The attitude control system during coasting periods is briefly described. The functional behavior and characteristic data of the main guidance and control hardware such as the inertial sensors, stabilized platform, digital computer, data adapter, control computer, and actuation system are described. Reliability requirements are emphasized. The principle of redundancy is extensively used to obtain highest reliability for long operating times. Data and results from recent Saturn I flights summarize the performance of the guidance schemes. -
Briefing for Apollo 10.
This document contains a transcript of the briefing meeting for the launch of Apollo 10. Participants include George H. Hage, Colonel Thomas McMullen, and William J. O'Donnell. -
"Nondestructive testing of space vehicle liquid propellant rocket engines."
Presented at the Western Metals Congress, Los Angeles, California, 15 March 1967.; Archive copy is a photocopy.; ABSTRACT: This report describes the various nondestructive test methods employed to evaluate materials and processes used in the manufacture of large liquid propellant rocket engines at the Rocketdyne Division of North American Aviation, Inc. The contents of the paper were purposely oriented for an audience of aerospace, design and materials engineers. A brief description of liquid propellant rocket engine reliability is presented. The relationship of standards and specifications to nondestructive testing is discussed and various test methods are described along with a discussion of their applications and limitations. The sequence of events leading up to the use of nondestructive testing in production inspection is presented. Finally, the organization of labor directly related to nondestructive testing is given. -
"Manned Launch Vehicle Development."
Includes handwritten notes. Includes references to slides. Essay remarking on how space vehicles will interact on the moon's surface. -
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Oral History Interview With Steven Hall
Steven Hall was born in a small town in the north central part of Indiana. This town has about a population of 2,000 people. Steven graduated from Eastern High School in 1963, and then he enrolled in Aeronautical/Neurospace Engineering at Purdue University. There, he received his bachelor's degree in 1968. Steven originally became interested in man space-flight when he was just about 10 years old. At this age, he had no clue how he could get involved with the space station, but he knew that he wanted to get involved one day. After he graduated college, he was so ready to work at NASA, that he left his home town immediately to move down to Huntsville, AL to start working. When he began working at the Marshall Space Flight Center, he was shown how Human Factors Engineering worked. One of the first projects that Steven was able to work on was "Skylab" where they built a lot of the equipment that probed how humans responded to space, and how the body changes in space. He also worked on a program to design a vehicle to drive around the surface of the moon.Tags Oral History -
