UAH Archives, Special Collections, and Digital Initiatives

Browse Items (1965 total)

  • Friday__February_16__2018_at_10_22_41_AM_default_86d15cc7.mp4

    As a kid, Charles M. Louis loved to take things apart and put them back together. He also was inspired as a kid while reading a Life magazine article with Wernher Von Braun standing next to the Saturn V engine at the age of 15. Since he was an avid Science Fiction reader at the time, this all inspired him to become involved with the Space Program, and to eventually become a licensed hand radio operator. In college, he pursued an Electrical Engineering degree, and he flunked out of college becasue the classes were too big. Because of this, he decided to change schools and go to the Detroit Institue of Technology. There, he was more successful because of the smaller class sizes. After graduating college, he was hired at Boeing in Seattle, Washington. At Boeing, he was involved in Test Engineering supporting UHF and Microwave antennas on the Minuteman Program. Boeing then got a contract for the Saturn V Program 8 months after Charles started working there. He decided he would rather work on the Space Program then the military side, so he decided to move down to Huntsville, AL to work on the program.
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  • Friday__March_9__2018_at_11_03_22_AM_default_5387bb7d.mp4

    Kim B. Robertson is a retired Design Engineer, and has lived in Huntsville, AL his whole life. He grew up in the Monte Santo Mountain area where most of the German scientists on Von Braun's missile team lived, so being involved with the Space Station was always a part of his life growing up. He knew from an early age that Huntsville was where he always wanted to live, and this is the area that he wanted to work in. Robertson eventually went to Auburn University where he was able to work on a Marshall project. He was able to work on the Industrial Design team there, and he, along with his group, was asked to do some design work to get ideas for Skylab and the Space Station. After graduating from Auburn, he joined the National Guard with a year of active duty. While being in the National Guard, he became a ground-radio maintenance technician. His first job in Huntsville was working at URS Matrix, and there he worked on the hand-controller for the shuttle arm. He also did some volumetric studies for putting experiments in the back part of the shuttle work-area.
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  • Friday__May_4__2018_at_12_10_52_PM_default_fb72b05a.mp4

    Joe Phillipauldy is originally from Central, New Jersey. He did his undergraduate training at the University of Richmond in Virginia, and then he received his Master's degree at Villanove University. He then when on to get his graduate degree, and completed the program in 1984. His degree was in Experimental Psychology. In 1986, he accepted a job position with the Creatis Systems Tech Staff at Boeing Military Airplanes in Kansas. His first Human Engineering job was with Tech Staff. A project he spent a lot of time on was the Airforce I VC25 747 Presidential Replacement Program. With this, he did a workload analysis of the navigator crew station. After this work, Joe got involved with the Human Factors and Industrial Applications group. There, he ran task terms around the factory floor doing analyses and reporting on ergonomics issues on assembling vehicles. Later, he was able to work on the Space Station Vehicle Integration Contract in Huntsville, AL.
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  • Friday__November_10__2017_at_11_59_55_AM_default_288347a7.mp4

    Dr. John Rogers is from Kansas, and in Kansas, John loved to drive out into the prarie and find places where there had been homesteads. There, he would lay on the ground and look up at the stars at night. This all inspired him to get involved with the space station, and human factors engineering. John received his Bachelor's degree at Kansas State University, and then he received his Master's degree at The University of Arkansas. At this point, he took up a teaching job in Arkansas, and during that period of time, he recieved a National Science Foundation summer research fellowship at Florida State University. There, John did research on the effects of radiation on the human body. After leaving his teaching job, he went to the University of Mexico to pursue his Phd. While he was there, he was able to be a part of a summer program that pushed him towards his career. Since John did such a great job at the summer program, they kept him on as a consultant where he could work unlimited hours, and work any time he wanted to. The work that he did there included: examining human air and organizations, and considering what was the common factor/the emphasis in the atomic energy. After his job there, he started working at NASA in June of 1967. His job tasks there included: looking at the simulations and to look at the experimental design. He also had to try to make sure that they had solid statistics behind their results that were being detained.
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  • Friday__November_17__2017_at_10_45_21_AM_default_182d3f85.mp4

    Charles Brian Nelson was born in 1938 in Memphis, Tennessee. He received his first degree in Industrial Design at Tennessee Tech. After he graduated from college in 1960, he went to work with the Depot Company where his job was making Titanium Dioxide. Charles stayed at this job for about 5 years, and by encouragement from his friends, he moved to Huntsville to work at NASA. He started out working at a test lab where they were responsible for getting the test bird into the test stand to test it. This job also included testing of vibrations, engine fire, and testing every individual part. After this job, Charles moved into the human factors engineering group. He worked for NASA for about 12 years.
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  • Friday__October_5__2018_at_9_33_54_AM_default_3ed44883.mp4

    George Hamilton has lived in Huntsville, Alabama all of his life, and his father was a Charter Marshall Member in Huntsville. When he was working, George's father was chosen as a "guinea pig" to go up in the Pregnant Guppy, which was a large, wide-bodied cargo aircraft. Because of George's father's career and interest with NASA, it made George interested in the career as well. George has a lot of family stories like this, which all have inspired him to take on his career that he has now. After high school, George went to The University of South Alabama in Mobile to study Marine Biology. Over the summer he had a change of heart, so he decided to transfer to Auburn University for Mechanical Engineering. After he finished up with his degree, he started working in small, manufacturing spare parts for missiles. After this career, he started to work at Avco Electronics in Huntsville where he worked at the plant on the design side. After this, Avco started looking for people to go overseas on the construction side of the house, so George went overseas with them. Then he came back, got married, and received his Phd in Biomedical Engineering at The University of Alabama in Birmingham.
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  • Friday__October_6__2017_at_12_18_03_PM_default_1dbb40e7.mp4

    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.
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  • Friday__October_20__2017_at_11_06_48_AM_default_8038320d.mp4

    Vigontus Kulpa grew up in Huntsville, AL. Ever since he was young, Kulpa was always interested with the space program. He ended up going to college at UAH, and was considered a "feter" co-op engineer, so he actually started out at The Marshall Space Flight Center. There, Kulpa worked with the Human Systems Integration Branch. In college, Kulpa started out at UAH, but eventually ended up graduating from college at Auburn University. He then came back to UAH to receive his Master's degree in Systems Engineering and his Doctorate in Psychology and Human Factors. Kulpa's first full-time assignment was as a Crew Procedures Engineer. In this job, he was considered "between" the scientists that did the experiments, and the astronauts. Kulpa ended up working with the Avionics group to design a battery-operated wrench, and he took this on the KC-135. He also was able to work to help re-design the space station. After a while, he switched jobs and worked with the Neutral-Buoyancy Tank where he worked on how to make a space shuttle suit work underwater.
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  • Friday__October_27__2017_at_12_12_20_PM_default_1fcc37b7.mp4

    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.
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  • Friday__September_8__2017_at_12_16_04_PM_default_2b1019c8.mp4

    Michael Bacato was born in Brooklyn, New York in 1927. When he started high school at the age of 14, Pearl Harbor was attacked by the Japanese. When he graduated high school, he enlisted in the Navy in 1945 so he wouldn't have to go into the Army. He stayed in the Navy for two years. In the Navy, Michael was on a crew of the Destroyer. When he got discharged from the Navy, he then started college in 1948. To help pay for college, he started working with the merch marines selling out oil tanks. He finished this in 1951. Michael started out in college at New York University, and soon after he almost had to go back to the Navy because North Korea invaded South Korea. To avoid going back, he joined the ROTC at NYU with the airforce. In 1952, he entered the extended active duty with the United States airforce as a second lieutenant. He went to Keesler Airforce Base for training, and he spent two years there. There, he became a Radar Officer. After his training, Michael then started to become interested with Von Braun, and the development of rockets in Huntsville, AL. He then finally made a decision to leave the airforce, and he moved to Huntsville to work. He went into the Mechanical Engineering Design group. One of the first projects he was assigned to was the life support system, working with two monkeys. He then was offered a job in the Bioengineering group, which he liked much better, so he decided to stay with this group. His last program he worked on was on the Hubble Telescope, where he had the opportunity to work with Buzz Aldron.
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  • Friday__September_15__2017_at_12_11_55_PM_default_69f7b692 (1).mp4

    After Robert McBrayer graduated college, he reported to the Johnson Space Center in March of 1963. He was there assigned to a section called "Biodynamics" and in that section, they worked on Human tolerances to impact sustaining acceleration and acoustics. Robert was assigned to the acoustics group, and his first job was to design and develop a machine to produce low-frequency pure tones to test humans. He also designed and developed a test chamber for testing humans, and he participated in doing the actual human test with the machines that he helped build. He helped document the results as well. After his venture in doing basic research, he went into an area called "crew's survival equipment design and development," and he was assigned pieces of equipment that were his to design, update, and help build. In 1966, Robert asked to be transferred from the Johnson Space Center to the Marshall Space Flight Center, and he then moved to Huntsville, AL. Robert was immediately put on the Orbital Workshop where they were writing task analysis, and procedures for crew station reviews. They did two of those, on in 1967 and the other in 1968. From the Orbital Workshop, he was responsible for all the crew interfaces on adapter, etc.
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  • Friday__September_21__2018_at_1_59_49_PM_default_89bca7ab.mp4

    Charles Dissinger was born and raised in Virginia. As a small child, Charles's father would drive him over to the Langley Research Center in Virginia, and he was always engaged with the space program. Charles remembers watching every space launch on tv with his dad as a kid. Being inspired by space, he decided to go to The University of Virginia to get his bachelor's degree in Biology. Then, after graduating, he taught high school for 4 years. After this, he went back to graduate school at West Virginia University to get his master's degree in Biology/Biochemistry. His second career after teaching, was doing Biochemical research for 19 years. Charles's wife later on received a job offer at The Marshall Space Flight Center in Hunstville, AL to join the Information Technology Organization there. She took this job, and they moved to Huntsville. Charles was then soon after hired in 1994 at NASA. His first project there included finding the requirements for the NASA Standard 3000 design. This project was called "The Launch Deployment Assembly" which was a system to deliver the robotic arm to the space station. Another program Charles was involved in was the Propulsion Module.
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  • Friday__September_28__2018_at_8_59_16_AM_default_b6b1e023.mp4

    Edwin Pruitt is from a small town in Alabama. He went to Auburn University, and when he was a sophomore there, he applied to a co-op position. In this co-op, he was assigned to a flight-dynamics group. Edwin was not satisfied with this position, so he asked to be switched to another one. In this new co-op, he was able to drive around on the simulated moon surface. Some things he was also involved in was diving into the Neutral Buoyancy Simulator, flying on the KC-135, and he had the freedom to represent his group with other part of the center where he worked. After Edwin graduated from college, he got a job at GE Aerospace in Valley Forge. They had a contract with the Airforce to train the Airforce astronauts. He eventually got laid off from this position, and he next got a job at Teledyne Brown Engineering. After working there for a couple of years, he found a job at Matrix in Huntsville. After working here, he found a job at Essex working on proposals.
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  • Friday__September_28__2018_at_10_34_25_AM_default_122089af.mp4

    Charles Van Valkenburg grew up in Huntsville, AL, and he went to Auburn University. There, he majored in Industrial Design and he had a part-time job as a draftsman at one of the civil engineering firms. After graduating college, he received a job at Essex in Huntsville. At this job, Charles would get in the water of the Neutral Buoyancy Tank and make sure that all the tools and everything was in place for an astronaut. Sometimes, he would even be the test subject. After all the testing from the day, they would all have a debriefing session at this company where the astronaut, human factors experts, and engineers would all make inputs. After the debriefing, they would take the ideas and get the machinists to make some modifications to the hardware. Charles would also work in pressure suits, and he explains how restricted the suit made him feel. He also mentions the foot restraints, and how difficult they were to work with. In his career, Charles was also able to help design the underwater version of the manned maneuvering unit.
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  • Friday__September_29__2017_at_11_29_57_AM_default_2a11bcb7.mp4

    Richard Heckmann was born in Ohio, and he lived there until he was 9 years old. When he turned 9, his dad received a civil engineering job in Washington D.C., so they moved there soon after. After this, they then moved to Maryland. Richard explains that he was a sickly child, and he was once in a coma for 10 days when he was just 7 years old. Growing up, he became more healthy and ended up going to Johns Hopkins University and graduated with an Engineering Science degree. Richard eventually accepted a commission in the ordinance corp, and he went to Fort Bliss for a guided missile school. He spent two years in the autillery there. At Fort Bliss, he received his private pilot's license while he was in the service. Then, they took Richard back to the ordinance corp. and they sent him down to the Redstone Arsenal, where he got stationed. After this career, Richard worked as a project engineer for the manufacturing for hardware at Thiokol. He then transferred to Hayes Industry, and he worked with the manufacturing engineering lab at the Marshall Space Flight Center. There, he worked on the Apollo Applications Program.
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  • Convenertranstel_011509130952.pdf

    One of the Orange Aid Preprint Series in Nuclear Astrophysics, September 1968.; Supported in part by the National Science Foundation [GP-7976], the Office of Naval Research [Nonr-220(47)]. ; ABSTRACT: The motion in a convectively unstable region is expanded into an ensemble of convective cells. Each of these cells interacts with the surrounding medium according to the semiempirical model proposed by Turner (1963 ). Possible detailed models of the flow patterns within each cell are presented. The radius and velocity of these cells are given as functions of distance moved. The convective flux and rms velocity are given as averages over the ensemble of cells. As in the standard mixing length theory the principle uncertainty remains the average initial radius of the cells.
  • Crewbrieinst_012309113213.pdf

    Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points.
  • uprsatIBquafilrepandrelmatfilsciforsatquafilrepno15_071007103723.pdf

    Unclassified film script of the Saturn I/IB Quarterly Film Report covering January, February, March, 1963. There are handwritten notes and edits throughout the document.
  • uprsatIBquafilrepandrelmatfilsciforsatquafilrepno16_071007104133.pdf

    Unclassified film script of the Saturn I/IB Quarterly Film Report covering April, May, June, 1963. There are handwritten notes and edits throughout the document.
  • uprsatIBquafilrepandrelmatfilsciforsatquafilrepno18_071007104903.pdf

    Unclassified film script of the Saturn I/IB Quarterly Film Report covering October, November, December, 1963. A handwritten note at the top of the title page lables this copy as the "Final Draft".
  • usaerospprog_081607135439.pdf

    The document contains four charts labeled "Investigation", "Exploration", "Utilization", and "Control". Each chart is organized chronologically, contains drawings of U.S. Aerospace Program Projects, and incudes written descriptions of each project.
  • Useoftankmounboospump_031607093838.pdf

    This paper outlines the results of a test program which was planned to demonstrate the feasibility of using a tank mounted, all-inducer, high speed liquid hydrogen booster pump to provide NPSH for the turbo pump in a reactor-powered vehicle. The cavitation problem associated with pumpoing liquid hydrogen, when used as a propellant, is further aggravated by localized heating caused by radiation from the reactor.
  • usessaturn_071607093947.pdf

    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.
  • variorgchartsabmadur19571960_031607111853.pdf

    Includes letter to Mr. David Christensen, University of Alabama Research Institute.
  • Vibracouenvichar_011509105838.pdf

    This paper presents representative examples of vibration and acoustic data from flights of the Saturn V launch vehicle and static firings of Saturn V launch vehicle stages. The purpose of the paper is to provide vibration and acoustic environment characteristics which are pertinent to the design of launch vehicles
  • visuaidlibr.pdf

    This document includes revisions. There are missing pages from page 237-238. This reference document catalogues all MSFC oriented visual aids filed in the Visual Aids Library of Marshall Space Flight Center. These visual aids are updated by the Graphic Engineering & Models Branch, Industrial Operations Program Management Information Office, and the Research and Development Operations Management Office. The purpose of the Visual Aids Library is to provide management data visuals in the form of slides (3 X 4 and 2 X 2), or black and white prints, to MSFC offices and laboratories, and other centers, who have a valid requirement. The visual aids are issued on a loan basis in order to obtain as wide a use for each visual and to assure that the latest revisions are incorporated in the issued item. Visuals may be ordered from the Visual Aids Library, located on the 10th floor of building 4200 (Phone 876-7237, 876-6960, 876-0983). In addition to the visuals published in this book, photographs from prime contractors are available from Industrial Operations, Program Management Information Office, Room 621, building 4201. Visuals with erroneous or obsolete information should be brought to the attention of the Visual Aids Library, preferably in writing, so that corrections can be made immediately. This publication will be kept current through distribution of pages of new visuals and notification will be made on obsolete visuals so they may be crossed out in the catalogue. Comments and suggestions concerning this publication will be greatly appreciated. Changes in the distribution lists should be directed to Mr. Gordon 0. Willhite, or Mrs. Opal Tabor, Visual Aids Library, MS-G.
  • Vonbraumoveende_072910160005.pdf

    The Huntsville Times
  • welcrymatforaerapp_121407125356.pdf

    Cryogenic propellant rocket engine hardware and the related test facilities will be described. Methods used for selection of alloys for liquid oxygen and liquid hydrogen service will be discussed. Unique equipment and welding procedures are reviewed with emphasis on welding problems and their solutions to assure reliable hardware and facilities. Examples of specific welding procedures and methods of quality assurance will be given for joining application ranging in size from .001" to 11" thick sections.
  • welforaerappapandis_060707142709.pdf

    Original is a photocopy; W. A. Wilson, Chairman; Russell Meredith, North American Aviation; Robert Hackman, Linde Company; Frank Wallace, Pratt-Whitney Aircraft; P.G. Parks, NASA, MSFC; G. O. Hoglund, Aluminum Company of America.
  • werewinntheracewithruss_032107081023.pdf

    Partial article discussing the United States' victories in the space-race over Russia.
  • wheregoingspacemgmt_062907110845.pdf

    Presented to the First Space Congress, Cocoa Beach, Florida, April 21, 1964 by Joseph H. Reed, Chief, Management Analysis Office, Executive Staff, Marshall Space Flight Center at the request of the Associate Administrator for Manned Space Flight, NASA
  • whyinternalinsulationforthesaturns-iv_041207133311.pdf

    Prepared for presentation at the Cryogenic Engineering Conference, Los Angeles, California, August 14-16, 1962.; There is no page 8.
  • xraytelinsofaerwel_060707140201.pdf

    A sensitive new television X-ray image enlargement system has been developed under sponsorship of Watertown Arsenal Laboratories (Army Materials Research Agency) by the Department of Welding Engineering of The Ohio State University. Now commercially-available through Philips Electronics Instruments (Norelco), complete systems have been in service since January 1963 in aerospace, electronic, and other facilities. Such users report highly- satisfactory performance and unusual reliability in service. The new X-ray system permits in-motion or stationary examination of critical aerospace materials, components, and systems such as sheet materials, weldments, brazed joints, electronic components, printed circuit assemblies, small mechanisms, and biological specimens.
  • zerostage_082707085507.pdf

    To meet the demands of increasing payload size and weight, and to fill the large payload gap between the Saturn IB and Saturn V, a number of methods of uprating the Saturn IB have been studied by NASA and Chrysler Corp. of providing increased payload capability is discussed in this paper. Four 120 in. United Technology Center UA-1205 solid propellant motors, originally developed for the Air Force Titan III program, are clustered around the S-IB first stage of the Saturn IB launch vehicle. These four solid propellant motors provide the total thrust for liftoff of the vehicle, with S-IB stage ignition occurring just prior to burn-out and separation of the solid propellant motors. The term "Zero Stage" is applied to this added stage.
  • TheNASAGrumApol_052410121955.pdf

    Handwritten in pencil on the document. Describes the layout and function of various sections of the Apollo lunar module.
  • Theoliqupropperf1.pdf

    Archive copy is a photocopy.; The purpose of these writings is to compile in one volume the basic elements of thermodynamics and gas dynamics which are useful in the evaluation of thrust chamber performance. It is presumed that the reader will have had an elementary course in thermodynamics and gas dynamics. The discussion of topics useful in evaluating thrust chamber performance is, of necessity, limited to these physical effects amenable to other areas that are as yet in the research stage of development. The author would like to take this opportunity to express his gratitude to Mr. G. S. Gill for many stimulating discussions on this subject. Thanks are due to Mr. D. J. Kuyper for permission to utilize his discussion on elastic-plastic strain and its application to nozzle throat area change. Finally, the author wishes to express his gratitude to his wife, Alice, who typed the bulk of the manuscript.
  • thepromanpro_020408133725.pdf

    Included in "First Annual Logistics Management Symposium," Huntsville, Alabama; Archive copy is a poor photocopy. Describes the stages of rocket-development/launch and the logistical problems with each.
  • theprooflartanforcryfue_071207131317.pdf

    Archive copy is a poor photocopy. Prepared for presentation at Deutsche Gesellschaft fur Raketentechnik und Raumfahrt. (German Society for Rocket Technology and Astronautics). Given by E. Harpoothian, Chief Engineer, Structures Department, Development Engineering.; Tanks for cryogenic fluids, as used in the Saturn space vehicles, have reached an advanced stage of design and development. Many of the structural features of the NASA/Douglas Saturn tanks, fabricated of 2014-T6 aluminum alloy, were first developed for the booster of the Thor ballistic missile, which later found extensive use in putting space vehicles into orbit. There is a mutual dependence of important factors related to design concepts, selection of materials, processing techniques, and fabrication methods. It is shown that this mutual dependence must be considered if a successful vehicle is to emerge from design and development. Details of vehicle structure, provision for insulation, and manufacturing methods are presented. Criteria for the selection of materials is shown to be dependent on strength, ductility, weldability, toughness, fabricability, behavior at cryogenic temperatures, and on manufacturing methods and inspection techniques.
  • ThermalModels_081108112916.pdf

    One of the orange Aid Preprint Series in Nuclear Astrophysics by W. B. Hubbard, California Institute of Technology, Pasadena, California.; Argues that the Saturnian models are flawed as their predictions do not line up with detected gravitational events.
  • Theroleofsimuinthedeveofanautochecsyst_110507111856.pdf

    For publication in Luftfahrttechnik Raumfahrttechnik. Discusses the uses and advantages to using simulations.
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