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  • 1
    Publication Date: 2006-01-12
    Description: The environmental control systems and system requirements of the Apollo command service module and the lunar module are described. The overall performance of both systems during the Apollo program is discussed. Other topics covered include: dust control, EVA provisions, Apollo 13 emergency, component redundancy, modular construction, and subatmospheric design.
    Keywords: AEROSPACE MEDICINE
    Type: Biomedical Results of Apollo; p 517-543
    Format: text
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  • 2
    Publication Date: 2019-07-13
    Description: Analytical studies of phase change effects in parallel and tapered liquid face seals are presented. An isothermal and adiabatic model of low Reynolds number flow are considered by numerical integration of the descriptive equations for a real fluid, and its thermodynamic properties are calculated for each step, using a computer program for the steam tables or fluid thermodynamic properties. It was shown that for low leakage rate the isothermal model is more accurate and for high leakage rates the adiabatic model is more accurate; that both models yield the same conclusions regarding stability; and that the transient of collapse is described by the adiabatic model which predicts a catastrophic collapse and then either failure or explosive return to a larger film thickness value. Finally, it is shown that converging seals may become unstable and the mass leakage rate is reduced significantly below the all liquid value when boiling occurs.
    Keywords: MECHANICAL ENGINEERING
    Type: ASME PAPER 79-LUB-4 , Lubrication Conference; Oct 16, 1979 - Oct 18, 1979; Dayton, OH
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Description: A study is made of boiling (or phase change) in liquid face seals. An appropriate model is set up and approximate solutions obtained. Some practical illustrative examples are given. Major conclusions are that (1) boiling may occur more often than has been suspected particularly when the sealed liquid is near saturation conditions, (2) the temperature variation in a seal clearance region may not be very great and the main reason for boiling is the flashing which occurs as the pressure decreases through the seal clearance, and (3) there are two separate values of the parameter film-thickness/angular-velocity-squared (and associated radii where phase change takes place) which provide the same separating force under a given set of operating conditions. For a given speed seal face excursions about the larger spacing are stable, but excursions about the smaller spacing are unstable, leading to a growth to the larger spacing or a catastrophic collapse.
    Keywords: MECHANICAL ENGINEERING
    Type: ASME PAPER 77-LUB-12
    Format: text
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  • 4
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    In:  Other Sources
    Publication Date: 2019-06-27
    Description: A cost analysis of a low-volume multiphasic health testing program is presented. The results indicate that unit costs are similar to those of high-volume automated programs. The comparability in unit cost appears to result from the savings in personnel and space requirements of the smaller program as compared with the larger ones.
    Keywords: AEROSPACE MEDICINE
    Type: Proc. of the Ann. Conf. of NASA Clinic Directors, Environ. Health Offic., and Med. Program Advisors; p 189-224
    Format: text
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  • 5
    Publication Date: 2019-06-27
    Description: A simplified computer program is presented which allows for the prediction of boiling (phase change) in liquid face seals. The program determines if and when boiling occurs and then calculates the location of the boiling interface, pressure and temperature profiles, and load. The main assumption which allows for a simplified analysis is the assumption of an isothermal gas phase.
    Keywords: MECHANICAL ENGINEERING
    Type: NASA-CR-134668
    Format: application/pdf
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