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  • Other Sources  (261)
  • AERODYNAMICS  (60)
  • STRUCTURAL MECHANICS  (57)
  • CHEMISTRY  (55)
  • THERMODYNAMICS AND COMBUSTION  (48)
  • AUXILIARY SYSTEMS  (41)
  • ASTROPHYSICS
  • 1970-1974  (261)
  • 1960-1964
  • 1972  (261)
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  • Other Sources  (261)
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  • 1970-1974  (261)
  • 1960-1964
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  • 1
    Publication Date: 2019-06-27
    Description: The molecular and atomic mechanisms for the hydrogen-iodine exchange reaction are treated theoretically by means of extensive classical trajectories calculated on a reasonable potential energy surface on which the single adjustable parameter is the iodine-core effective charge. The analysis shows the molecular mechanism to be dynamically forbidden, but gives an over-all rate constant for the atomic mechanism that is in agreement with the experimental values. It is indicated that the formation of a weak H2I complex plays an important dynamical role if the atomic mechanism is limited to reactions with collision complexes involving no more than two hydrogen atoms and two iodine atoms. Excellent agreement with experiment is obtained for the rate constant for the recombination I+I+H2 yields I2+H2 and its negative temperature coefficient.
    Keywords: CHEMISTRY
    Type: Journal of Chemical Physics; 56; June 15
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  • 2
    Publication Date: 2011-08-16
    Description: Measurement of the N2 concentration and temperature, the ion composition and concentrations, and the electron temperature up to 290 km about 30 and 5 min before totality during the Mar. 7, 1970, eclipse. The rockets traveled similar trajectories, thus permitting the purely temporal changes between flights to be resolved. The neutral temperature and N2 concentration changed little, but the electron temperature decreased by as much as 20% in the lower F region. The ion concentration decreased by about 30% in the F region and about 50% in the E region, with little change in relative ion composition. The electron cooling rates decreased by a factor of 6 in the lower F region, approximately in proportion to the change in the visible solar disk. A smaller than expected decrease in the cooling rate below 150 km between the two flights indicates a hardening of the solar spectrum and suggests a significant heat contribution from the solar corona near totality. The ion composition measurements were consistent with solutions of the ion continuity equations. A proper fit required a factor-of-three enhancement of the flux below 200 A, an amount also consistent with the electron heat balance analysis. Reactions involving the minor ions N(+) and N2(+) were found to be important for the ion chemistry of the major ions O2(+) and NO(+), especially at the time of eclipse.-
    Keywords: CHEMISTRY
    Type: Journal of Atmospheric and Terrestrial Physics; 34; Apr. 197
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  • 3
    Publication Date: 2011-08-16
    Keywords: CHEMISTRY
    Type: Biochemistry; 11; 15, 1; 1972
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  • 4
    Publication Date: 2011-08-16
    Description: The observation of 'double quantum' transitions which made it possible to determine the charge state of Ti as 2+ is reported. The EPR spectrum observed at 1.2 K is presented in a graph. The first derivative of the absorption is shown vs the magnetic field. The hyperfine patterns for the Ti-47 and Ti-49 isotopes are identified. Spin-Hamiltonian parameters for Ti(2+) in various cubic hosts are listed.
    Keywords: CHEMISTRY
    Type: Journal of Chemical Physics; 57; Oct. 15
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  • 5
    Publication Date: 2019-06-27
    Description: An experimental study of phase equilibria in the He-CH4 system was carried out over the temperature range 95 to 290 K and at pressures to 10,000 atm. The experimental results consist of equilibrium phase composition for twenty-eight isotherms in the region of coexistence of two fluid phases, together with the pressure-temperature trace of the three-phase boundary at which a CH4-rich solid phase is in equilibrium with the two fluid phases. The system exhibits a fluid-fluid phase separation which persists to temperatures and pressures beyond the range of this experiment. These results, together with those recently obtained for other binary systems, provide information about the form of phase diagrams for binary gas mixtures in the region of pressure induced phase transitions at high pressures. These findings are relevant to problems of deep atmosphere and interior structures in the outer planets.
    Keywords: CHEMISTRY
    Type: Univ. Space Res. Assoc. High Pressure Phys. and Planetary Interiors; p 69-77
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  • 6
    Publication Date: 2019-06-27
    Keywords: CHEMISTRY
    Type: Journal of Electroanalytical Chemistry and Interfacial Electrochemistry; 38; 1972
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  • 7
    Publication Date: 2019-06-27
    Keywords: CHEMISTRY
    Type: Earth and Planetary Science Letters; 17; Dec. 197
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  • 8
    Publication Date: 2019-06-27
    Description: Fourteen C-130 airplane center wings, each containing service-imposed fatigue damage resulting from 4000 to 13,000 accumulated flight hours, were tested to determine their fatigue crack propagation and static residual strength characteristics. Eight wings were subjected to a two-step constant amplitude fatigue test prior to static testing. Cracks up to 30 inches long were generated in these tests. Residual static strengths of these wings ranged from 56 to 87 percent of limit load. The remaining six wings containing cracks up to 4 inches long were statically tested as received from field service. Residual static strengths of these wings ranged from 98 to 117 percent of limit load. Damage-tolerant structural design features such as fastener holes, stringers, doublers around door cutouts, and spanwise panel splices proved to be effective in retarding crack propagation.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-CR-2075 , ER-11178
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  • 9
    Publication Date: 2019-06-27
    Description: Selected system supporting analyses in conjunction with the preliminary design of an auxiliary power unit (APU) for the space shuttle are presented. Both steady state and transient auxiliary power unit performance, based on digital computer programs, were examined. The selected APU provides up to 400 horsepower out of the gearbox, weighs 227 pounds, and requires 2 pounds per shaft horsepower hour of propellants.
    Keywords: AUXILIARY SYSTEMS
    Type: NASA-CR-1996 , REPT-71-7300-3.2-VOL-4
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  • 10
    Publication Date: 2019-06-27
    Description: Detailed cycle steady-state performance data are presented for the final auxiliary power unit (APU) system configuration. The selection configuration is a hydrogen-oxygen APU incorporating a recuperator to utilize the exhaust energy and using the cycle hydrogen flow as a means of cooling the component heat loads. The data are given in the form of computer printouts and provide the following: (1) verification of the adequacy of the design to meet the problem statement for steady-state performance; (2) overall system performance data for the vehicle system analyst to determine propellant consumption and hydraulic fluid temperature as a function for varying mission profiles, propellant inlet conditions, etc.; and (3) detailed component performance and cycle state point data to show what is happening in the cycle as a function of the external forcing functions.
    Keywords: AUXILIARY SYSTEMS
    Type: NASA-CR-1997 , REPT-71-7300-3.3
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