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  • 1
    Publication Date: 2005-11-30
    Description: Material removed from the spacecraft and returned to earth remained on the lunar surface for 31.9 lunations. None of the returned parts received the maximum 10,686 hours of exposure because of shadowing by the planar array antenna, solar panel, thermal control compartments, or other parts of the spacecraft. To determine the actual exposure of specific parts to sunlight, six series of photographs were taken. A one-fifth-scale model spacecraft was oriented to a collimated light source simulating the orientation of Surveyor with the sun. Three cameras were set up to view different parts of the spacecraft. The data obtained from these photographs permitted an evaluation of the effects of exposure to solar radiation on the camera and its parts, the surface sampling scoop, and the strut from the radar altimeter and Doppler velocity sensor.
    Keywords: SPACE SCIENCES
    Type: NASA, Washington Analysis of Surveyor 3 Mater. and Phot. Returned by Apollo 12; p 253-260
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  • 2
    Publication Date: 2005-11-30
    Description: The Surveyor 3 material analysis plan is composed of a series of comprehensive charts of all science and engineering investigations reported. The plan progresses from left to right on each figure. Each test was designed to ensure that the subsequent tests would not be significantly affected by those that preceded it. Each box represents one or more tasks performed by the individual or firm named at the lower left. The upper-right corner shows the amount and type of material subjected to the test or tests listed within the box.
    Keywords: SPACE SCIENCES
    Type: NASA, Washington Analysis of Surveyor 3 Mater. and Phot. Returned by Apollo 12; p 261-277
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  • 3
    Publication Date: 2005-11-30
    Description: The mirror on the Surveyor 3 television camera was subjected to tests which modified its surface. Lunar dust was removed by rubbing, by acetate and metallic film stripping techniques, rinsing, scraping, and by inadvertently touching the surface. A second shadow line was revealed. Second and third generation peels were taken across the upper shadow line, and a study was made in order to define the source(s) or events(s) responsible for creating the two shadow lines occurring on the lower part of the mirror.
    Keywords: SPACE SCIENCES
    Type: NASA, Washington Analysis of Surveyor 3 Mater. and Phot. Returned by Apollo 12; p 51-59
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  • 4
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    In:  CASI
    Publication Date: 2005-11-30
    Description: A summary is presented of the engineering and scientific results derived from the investigations conducted on the returned Surveyor 3 hardware, lunar soil, and photographs taken by the Apollo 12 astronauts.
    Keywords: SPACE SCIENCES
    Type: NASA, Washington Analysis of Surveyor 3 Mater. and Phot. Returned by Apollo 12; p 9-13
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  • 5
    Publication Date: 2006-10-26
    Description: Mark 1 X-ray tube operation at high temperatures to determine maximum temperature limit for operation in lunar X-ray diffractometer
    Keywords: ELECTRONIC EQUIPMENT
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  • 6
    Publication Date: 2006-10-26
    Description: Quartz and beryllium peak diffraction parameters as function of beryllium foil temperature
    Keywords: PHYSICS, GENERAL
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  • 7
    Publication Date: 2006-10-26
    Description: Reflection characteristics of beryllium window sample cups
    Keywords: PHYSICS, GENERAL
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  • 8
    Publication Date: 2006-10-26
    Description: X-ray diffraction profiles from beryllium window sample cups
    Keywords: PHYSICS, GENERAL
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  • 9
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    In:  CASI
    Publication Date: 2004-10-30
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: V-Gram: Magellan Quarterly Bulletin about Venus and the Radar Mapping Mission, Issue 9; p 1-3
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  • 10
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    In:  Other Sources
    Publication Date: 2018-12-01
    Description: Lunar rock petrography by X-ray diffraction system in soft-landed unmanned spacecraft
    Keywords: INSTRUMENTATION AND PHOTOGRAPHY
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