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  • Polymer and Materials Science  (17)
  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (15)
  • 1975-1979  (32)
  • 1
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    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: The thermal design work completed for the Thermal Protection System (TPS) of the Space Shuttle System (TPS) of the space shuttle vehicle was documented. This work was divided into three phases, the first two of which reported in previous documents. About 22 separate tasks were completed in phase III, such as: hot gas facility (HGF) support, guarded tank support, shuttle external tank (ET) thermal design handbook support, etc.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-144185 , LMSC-HREC-TR-D496704
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-27
    Description: The drift rates of the attitude control gyros onboard the Viking Orbiters were calibrated several times during flight. The calibration was performed by engaging the gyro control of attitude for a six-hour period, recording the Viking Orbiter coordinates of the sun and the roll reference star as a function of time, and processing these data by a computer program. The computer program calculated drift rates for each data increment, and then smoothed the calculated rate versus the time function for all the data on the basis of a Gauss-Markov gyro-drift model. The effects of data noise were minimized by using a relatively long time constant in the Gauss-Markov model and by empirically determining a set of corrections for celestial inertial scale factor error differences. In this way the rms error of the data fit was lessened.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Astrodynamics Specialist Conference; Sept. 7-9, 1977; Jackson Hole, WY; US
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  • 3
    Electronic Resource
    Electronic Resource
    Weinheim : Wiley-Blackwell
    Materialwissenschaft und Werkstofftechnik 6 (1975), S. 361-367 
    ISSN: 0933-5137
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Description / Table of Contents: The Use of Titanium Castings to Produce a Complex Shaped Intermediate Casing of RB 199.This paper describes the present position on a highly stressed casing and its functions in the RB 199-34 R engine. When the parts of the casing are made from solid forged titanium billets, up to 93% of the material used is machined away. For this reason, the most complicated parts of the casing were procured as castings and welded together by TIG welding. The paper describes the present quality standard of the titanium castings. The tests on the materials and their mechanical properties show that the castings are inferior to the forgings only with respect to their HCF behaviour and their elongation at rupture. Macroscopic flaws are not entirely inevitable but can be detected by X-ray tests. The future prospects for titanium castings are considered favourable.
    Notes: Der Bericht beschreibt die Lage eines hochbeanspruchten Gehäuses und dessen Funktionen im Triebwerk RB 199-34 R. Bei der Herstellung der Einzelteile des Gehäuses aus massiv geschmiedeten Titanblöcken wird bis zu 93% des eingesetzten Materials zerspant. Die kompliziertesten Partien des Gehäuses wurden deshalb als Gußteil bezogen und mittels WIG-Schweißung verbunden. Der Bericht beschreibt den heutigen Qualitätsstand der Titangußteile. Die Ergebnisse der Werkstoff- und Festigkeitsuntersuchungen weisen nur im HCF-Verhalten und der Bruchdehnung Nachteile des Gusses gegenüber dem geschmiedeten Material aus. Makroskopische Fehler sind nicht vollständing vermeidbar, aber durch Röntgenprüfung nachzuweisen. Die künftigen Aussichten des Titangusses werden positiv beurteilt.
    Additional Material: 14 Ill.
    Type of Medium: Electronic Resource
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  • 4
    ISSN: 0006-3525
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Notes: Conformational transitions induced by pH changes in random copolymers of leucine and glutamic acid have been studied. Significant differences were observed in the potentiometric titration curves of copolymers with small (up to 4%) and large leucine contents. The helical stability of copolymers with small leucine content, determined from titration curves by the Zimm and Rice method, decreases slightly with an increase in the leucine content, whereas the helical stability of copolymers with large leucine content increases sharply with an increase of the leucine content. It is shown that copolymers with large leucine content aggregate in the region of transition into the helical state, but the increase of their helical state stability is not connected with intermolecular aggregation, as it was also observed for a nonaggregating fraction isolated from one of the copolymers by gel chromatography. A conclusion is made that the helix-coil equilibrium constant s for leucine does not itself exceed the s constant for uncharged polyglutamic acid. The stabilization of the helical state in copolymers with large leucine content is due to intramolecular aggregation of helices in these copolymers. The analysis of the leucine residue distribution between helical and nonhelical regions in globular proteins also gives no real arguments to ascribe special helix-forming properties to leucine.
    Additional Material: 5 Ill.
    Type of Medium: Electronic Resource
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  • 5
    Publication Date: 2011-08-17
    Description: The International Ultraviolet Explorer (IUE) is a geosynchronous scientific satellite that was conceived as an international space observatory capable of measuring UV spectra of faint celestial bodies. Simple operational procedures allow the astronomers to joystick the spaceborne telescope about the sky, using familiar ground-based observatory techniques. The present paper deals with the IUE project objectives, the technical problems, constraints, trade-offs, and the problem solving techniques used in the IUE program.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 6
    Publication Date: 2019-06-27
    Description: The effects of photoelectron space charge and current density on differentially charged spacecraft are studied. The steady-state potentials of a sunlit cylinder are calculated using a two-dimensional computer code with a fully self-consistent treatment of space charge and an effective surface conductivity treatment of photoelectron currents. It is found that under conditions of strong differential charging the results do not differ greatly from NASCAP results, which neglect photosheath space charge and currents.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
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  • 7
    Publication Date: 2019-06-27
    Description: The reported investigation had the objective to illustrate the presence of important multidimensional effects in spacecraft charging. Two-dimensional codes have been under development by Parker (1976). A description is presented of a calculation which was performed using the three-dimensional NASA Charging Analyzer Program (NASCAP). NASCAP was run to calculate the electrostatic potentials on the surface of, and in the space surrounding, a sunlit Teflon-coated sphere. Currents to the sunlit surfaces were determined on the basis of an approximate photosheath model for strong differential charging.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Format: text
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  • 8
    Publication Date: 2019-06-27
    Description: The results are presented of a force test of a .88 percent scale model of the 142 inch solid rocket booster without protuberances, conducted in the MSFC high Reynolds number wind tunnel. The objective of this test was to obtain aerodynamic force data over a large range of Reynolds numbers. The test was conducted over a Mach number range from 0.4 to 3.5. Reynolds numbers based on model diameter (1.25 inches) ranged from .75 million to 13.5 million. The angle of attack range was from 35 to 145 degrees.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-144617 , DMS-DR-2277
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  • 9
    Publication Date: 2019-06-27
    Description: For abstract, see N76-16132.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-141826 , DMS-DR-2165-VOL-4
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  • 10
    Publication Date: 2019-06-27
    Description: For abstract, see N76-16132.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-141827 , DMS-DR-2165-VOL-5
    Format: application/pdf
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