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Jim McBarron has over 50 years of experience with NASA spacesuit development and operations as well as the U.S. Air Force pressure suit. As a result of his experience and research, he shared his significant knowledge about early Apollo spacesuit development, A-7L suit requirements, and design details.
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Configuration and systems description of life support equipment for intravehicular and extravehicular activity - Vol. 1
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This volume provides familiarization information essential to the operation of the extravehicular mobility unit (EMU), and describes the configuration combinations for the ATLB separable-components and the accessory contract end items. Configuration deviations may be made as dictated by specific crew/mission requirements. Operational procedures and malfunction detection procedures are found in Volume II of this handbook.
This report contains the results of additional studies which were conducted to confirm the conclusions of the MSC Mission Report and contains analyses which were not completed in time to meet the mission report deadline. The LM IMU data were examined during the lunar descent and ascent phases. Most of the PGNCS descent absolute velocity error was caused by platform misalignments. PGNCS radial velocity divergence from AGS during the early part of descent was partially caused by PGNCS gravity computation differences from AGS. The remainder of the differences between PGNCS and AGS velocity were easily attributable to attitude reference alignment differences and tolerable instrument errors. For ascent the PGNCS radial velocity error at insertion was examined. The total error of 10.8 ft/sec was well within mission constraints but larger than expected. Of the total error, 2.30 ft/sec was PIPA bias error, which was suspected to exist pre-lunar liftoff. The remaining 8.5 ft/sec is most probably satisified with a large pre-liftoff planform misalignment.
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There are no author-identified significant results in this report.
There are no author-identified significant results in this report.
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U-Th-Pb analyses of bulk samples of soil breccia 70019, when compared to KREEP data, indicate that different lunar samples are sometimes characterized by distinctly different initial Pb isotopic compositions. U-Th-Pb analyses on nonglassy samples and a glassy separate of soil breccia 70019, and bulk and agglutinate samples of soil 72701 showed that the glassy samples did lose considerable Pb relative to U less than 200 million years ago. These data support the contention of other investigators that vaporization of volatile elements owing to impact events significantly alters the chemistry of the lunar regolith. Metaclastic rock 60315 was reanalyzed and was found to be concordant at 3.93 billion years rather than slightly discordant, as was previously reported.
A15 and A17 primitive picritic glasses have been examined by FTIR for the presence of dissolved C-O species to determine the role of C-O gasses on driving lunar fire-fountains. A15 green and yellow glasses were extensively studied and found to be free of dissolved C species down to FTIR detection limits (10-100 ppm; species and sample specific). Preliminary data on A17 orange glasses are similarly devoid of FTIR detectable C-O species. Re-analyses of the C-O driving mechanism theory for mare volcanism demonstrates the need to determine the fO2 of the lunar interior; the factor that most critically determined the role of C gasses in the fire-fountaining events. Oxygen fugacities equivalent to IW-0.5 and above imply dissolved CO3(=) in the primitive glasses at levels above FTIR detection. The f02's below IW-0.5 imply concentrations of CO3(=) below FTIR detection. Recent data suggesting lunar mantle fO2's of IW-2 or less, strongly mitigate against finding FTIR measurable dissolved CO3(=) consistent with the findings of this study.