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  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (1)
  • intracellular symbiotes  (1)
  • 1
    ISSN: 1573-1561
    Keywords: Ergosta-5,7,24(28)-trien-3β-ol ; trienol ; intracellular symbiotes ; steroidogenesis ; planthoppers ; Nilaparvata lugens ; Laodelphax striatellus ; Homoptera ; Fulgoridae ; steroid-deficient diet
    Source: Springer Online Journal Archives 1860-2000
    Topics: Biology , Chemistry and Pharmacology
    Notes: Abstract Ergosta-5,7,24(28)-trien-3β-ol (trienol)6 was isolated from the intracellular symbiotes (symbiotic microorganisms) of the planthoppers,Nilaparvata lugens andLaodelphax striatellus. The steroidogenic end product of the symbiotes was found to depend on the environmental conditions, i.e., although trienol6 was produced under symbiotic conditions, ergosterol4 was formed in aerobic culture. When the normal diet was replaced by a steroiddeficient artificial one, the ratio of 24-methylenecholesterol5 to total insect sterols was significantly increased. The above study offers further corroborating evidence for our assumption that the host insects require 24-methylenecholesterol5 as an alternate source for cholesterol1 under certain environmental conditions. In our previous biotransformation experiments, 24methylenecholesterol5 was shown to be an immediate precursor of cholesterol1. However, the complexity of the insects' vital functions hindered all subsequent attempted transformations into cholesterol1 of sitosterol2, trienol6, and ergosterol4, under injection conditions.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-08-28
    Description: Space Station Freedom will be a platform for microgravity research. For superior microgravity science, the experiment locations must experience very little acceleration in the quasi-steady, structural dynamic, and vibroacoustic frequency ranges. This paper presents the methods that were developed for evaluation of the microgravity environment in the structural dynamic range. An integrated finite element model of the space station was used to conduct analysis for the on-orbit microgravity environment. Methods were developed to evaluate sinusoidal, random, and transient disturbances. Sources of disturbances aboard the Space Station were quantified and forcing functions were assembled. The resulting acceleration levels at the experiment locations due to these disturbances were computed and assessed against the microgravity acceleration requirement curve.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 93-1663 , In: AIAA(ASME)ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pt. 6 (A93-33876 1; p. 3332-3341.
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