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  • 1
    Electronic Resource
    Electronic Resource
    Amsterdam : Elsevier
    Phytochemistry 29 (1990), S. 3749-3754 
    ISSN: 0031-9422
    Keywords: Brachythecium rutabulum, B. salebrosum ; Eurhynchium striatum ; Rhytidiadelphus squarrosus, R. triquetrus ; Scleropodium purum ; arachidonic acid ; eicosapentaenoic acid. ; lipids ; mosses
    Source: Elsevier Journal Backfiles on ScienceDirect 1907 - 2002
    Topics: Biology , Chemistry and Pharmacology
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-07-13
    Description: High performance satellites and critical surfaces aboard advanced long-life spacecraft require effective contamination control measures to maintain performance stability and to ensure data accuracy. Contamination is said to exist and be of concern if a spacecraft or launch vehicle produced material interferes with the intended performance of a surface or sensor. This paper will discuss the development of contamination requirements for spaceborne optical instrumentation. In addition, a comparison of instrument contamination requirements to measured instrument degradation levels for mission activities will be presented. If maintained, these requirements ensure against undesirable instrument degradation due to the contamination environment created by fabrication, launch, mission activities, ambient atmosphere and the instruments themselves.
    Keywords: SPACECRAFT INSTRUMENTATION
    Type: Optical system contamination: Effects, measurement, control; May 19, 1987 - May 22, 1987; Orlando, FL; United States
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: A Scientific Instrument Protective Enclosure (SIPE) was designed to accommodate second generation science instruments (SIs) for the Hubble Space Telescope (HST) First Servicing Mission (FSM). One of the main design drivers for the SIPE is to provide a protective environment for the SIs against particulate and molecular contaminants that pose a viable threat to the SI performance. The focus of this paper will detail the methodology incorporated in the design of the SIPE to provide a controlled environment for SI protection at the launch site, during pre-launch/launch activities, and during on-orbit operations in the Shuttle bay.
    Keywords: SPACECRAFT INSTRUMENTATION
    Type: AIAA PAPER 93-1102 , ; 7 p.|AIAA, AHS, and ASEE, Aerospace Design Conference; Feb 16, 1993 - Feb 19, 1993; Irvine, CA; United States
    Format: text
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