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  • 1
    facet.materialart.
    Unknown
    Development of advanced composite rocket motor chambers using boron and graphite fibers. (1973)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Four 71-cm-diameter rocket motor chambers were designed and fabricated with advanced composite materials. The first three chambers were filament wound from boron/epoxy tape, and the fourth from graphite/epoxy tape. The first boron/epoxy chamber was 74 cm in length and was successfully hydroburst tested. The other three chambers were 57.6 cm in length for a smaller propellant load. The first shortened boron/epoxy chamber failed in proof test as a result of fabrication deficiencies. The last boron/epoxy and the graphite/epoxy chambers were successfully proof tested.
    Keywords: MATERIALS, NONMETALLIC
    Type: Conference on Reinforced Plastics in Aerospace Applications; Apr 05, 1973 - Apr 06, 1973; London
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Fabrication of boron/epoxy rocket motor chambers. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Three 71-cm-diameter boron/epoxy composite rocket motor chambers were filament wound. The first chamber was hydrostatically tested; the second failed in proof test as a result of fabrication deficiencies. The third chamber obtained a successful proof test, but deformed later in processing because of hydrolysis. In spite of the deformation, this chamber was test fired and then burst tested.
    Keywords: MATERIALS, NONMETALLIC
    Type: National Technical Conference and Exhibition; Oct 17, 1972 - Oct 19, 1972; Palo Alto, CA
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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