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09/27/07 - Class 428 site info Info monitor Monitor Keywords monitor archive Archive organizer Organizer account info Account |  Prev - Next

Low-density ablative heat shield fabrication pdficon_sm

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Abstract: Spacecraft heat shields are fabricated as one-piece assemblies using low-density ablative thermal protection materials. The heat shield assembly is built from modular pieces formed by ablative impregnation processing. Once the full-size heat shield is assembled from the modular blocks, heat treatment is used to bond the individual blocks together by facilitating polymeric cross-linking of impregnant material within and/or between each block. This provides a structurally integral one-piece heat shield assembly that can be further machined to final dimensions and attached directly to a spacecraft structure or a carrier panel separately attached to the spacecraft ...

Agent: John P. Wooldridge, Esq. - Kihei, HI, US
Inventors: M. Alan Covington, Margaret M. Stackpoole
USPTO Applicaton #: #20070224407 - Class: 4282921 (USPTO)

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Related Terms: Pregnant   Spacecraft   
The Patent Description & Claims data below is from USPTO Patent Application 20070224407, Low-density ablative heat shield fabrication.

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Pregnant   Spacecraft   


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