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  • 1
    facet.materialart.
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    In:  Other Sources
    Publikationsdatum: 2019-07-13
    Beschreibung: A procedure of fabricating graphite epoxy columns used in the assembly of large space platforms is described. The requirement for precise dimensional control led to a unique hot resin injection process. Dry, high modulus fiber is wound over a vertically mounted steam-heated mandrel. A steam-heated sleeve or caul is slipped over the wound mandrel and resin is injected and cured in place. Approximately 200 column elements have been fabricated using this efficient process.
    Schlagwort(e): ASTRONAUTICS (GENERAL)
    Materialart: Composite structures; Sep 16, 1981 - Sep 18, 1981; Paisley
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 2
    Publikationsdatum: 2019-06-27
    Beschreibung: Liquid propellant behavior under space flight conditions and predicting Apollo spacecraft liquid stability
    Schlagwort(e): PROPELLANTS
    Materialart: NASA-CR-92084 , LMSC-A874728
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
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  • 3
    Publikationsdatum: 2019-07-13
    Beschreibung: A simple, fully automatic assembler associated with the on-orbit assembly of tetrahedral truss platforms erected of graphite epoxy tapered columns is described. The assembler, which can operate either as a free flyer or attached to the Orbiter, is capable of constructing a platform from a full load of truss columns and node joints in 36 hours. The geometry of this electrically-driven machine is based on a compound parallelogram system which permits backward as well as lateral translations. Concepts have been developed for half-column assembly as well as for column and node joint insertion into the platform.
    Schlagwort(e): ASTRONAUTICS (GENERAL)
    Materialart: AIAA PAPER 81-0446 , Conference on Large Space Platforms: Toward Permanent Manned Occupancy of Space; Feb 02, 1981 - Feb 04, 1981; San Diego, CA
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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