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  • Other Sources  (1,084)
  • AUXILIARY SYSTEMS  (1,084)
  • 1970-1974  (1,084)
  • 1940-1944
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  • Other Sources  (1,084)
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  • 1
    Publication Date: 2005-11-30
    Description: Test results for thermal vacuum and radiation environment simulation of hydrazine contamination are discussed. Solar cell performance degradation, measured by short circuit current, is presented in correlation with the variations used in environmental parameters.
    Keywords: AUXILIARY SYSTEMS
    Type: Space Simulation; p 461-468
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  • 2
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Minute deflection actuators for optical mirror assembly
    Keywords: AUXILIARY SYSTEMS
    Type: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 303-306
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  • 3
    Publication Date: 2005-11-27
    Description: Gearhead electric motor choices for spacecraft boom deployment applications
    Keywords: AUXILIARY SYSTEMS
    Type: JPL PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 47-49
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  • 4
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Thermoelectric generators, solar cells, and primary cells for spacecraft power supplies
    Keywords: AUXILIARY SYSTEMS
    Type: SPACE PROGRAMS SUM. NO. 37-61, VOL. 3 28 FEB. 1970; P 130-148
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  • 5
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Description of scan actuator geared servomechanism for Mariner Mars 1969 spacecraft
    Keywords: AUXILIARY SYSTEMS
    Type: PROC. OF THE 4TH AEROSPACE MECH. SYMP. 15 JAN. 1970; P 103-111
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  • 6
    Publication Date: 2006-02-22
    Description: The lifetime of separator membranes currently employed in the electrolyte environment of silver-zinc batteries was estimated at 3 to 5 years. The separator membranes are crosslinked polyethylene film containing grafted poly (potassium acrylate)(PKA), the latter being the hydrophilic agent which promotes electrolyte ion transport. The lifetime was estimated by monitoring the rate of loss of PKA from the separators, caused by chemical attack of the electrolyte, and relating this loss rate to a known relationship between battery performance and PKA concentration in the separators.
    Keywords: AUXILIARY SYSTEMS
    Type: JPL Quarterly Tech. Rev., Vol. 2, No. 1; p 72-81
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  • 7
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    In:  CASI
    Publication Date: 2006-02-22
    Description: One of the most significant problems encountered in the use of silicon solar cells in space is the sensitivity of the device to electron and proton radiation exposure. The p-diffused-into-n-base solar cells were replaced with the more radiation tolerant n-diffused-into-p-base solar cells. Another advancement in achieving greater radiation tolerance was the discovery that the addition of lithium to n-base silicon resulted in what appeared to be annealing of radiation-induced defects. This phenomenon is being exploited to develop a high efficiency radiation resistant lithium-doped solar cell. Lithium-doped solar cells fabricated from oxygen-lean and oxygen-rich silicon were obtained with average initial efficiencies of 11.9% at air mass zero and 28 C, as compared to state-of-the-art n-p cells fabricated from 10 ohm cm silicon with average efficiencies of 11.3% under similar conditions. Lithium-doped cells demonstrated the ability to withstand three to five times the fluence of 1-MeV electrons before degrading to a power equivalent to state-of-the-art solar cells. The principal investigations are discussed with respect to fabrication of high efficiency radiation resistant lithium-doped cells, including starting material, p-n junction diffusion, lithium source introduction, and lithium diffusion.
    Keywords: AUXILIARY SYSTEMS
    Type: JPL Quarterly Tech. Rev., Vol. 2, No. 1; p 29-36
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  • 8
    Publication Date: 2006-02-22
    Description: A preliminary study of maximum power utilization methods was performed for an outer planet spacecraft using an ion thruster propulsion system and a solar array as the primary energy source. The problems which arise from operating the array at or near the maximum power point of its 1-V characteristic are discussed. Two closed loop system configurations which use extremum regulators to track the array's maximum power point are presented. Three open loop systems are presented that either: (1) measure the maximum power of each array section and compute the total array power, (2) utilize a reference array to predict the characteristics of the solar array, or (3) utilize impedance measurements to predict the maximum power utilization. The advantages and disadvantages of each system are discussed and recommendations for further development are made.
    Keywords: AUXILIARY SYSTEMS
    Type: JPL Quarterly Tech. Rev., Vol. 2, No. 1; p 37-48
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  • 9
    Publication Date: 2006-04-25
    Description: Third electrode and recombination electrode in nickel cadmium battery system of spacecraft
    Keywords: AUXILIARY SYSTEMS
    Type: NIFICANT ACCOMPLISHMENTS IN SCI. AND TECHNOL. AT GODDARD SPACE FLIGHT CENTER 1970; P 233-237
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  • 10
    Publication Date: 2006-04-25
    Description: Voltage converter/regulator for primary and secondary power sources in deep space missions
    Keywords: AUXILIARY SYSTEMS
    Type: NIFICANT ACCOMPLISHMENTS IN SCI. AND TECHNOL. AT GODDARD SPACE FLIGHT CENTER 1970; P 229-232
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