NASA NTRS ยท 20120016380
Thermal protection system and related methods
Abstract
A thermal protection system and a method of manufacturing are disclosed. The thermal protection system may be configured to protect a movable joint, for example, a flexible bearing of a rocket motor nozzle. The thermal protection system includes a series of annular shims separated by a plurality of discrete spacers. Each shim of the series of annular shims may have a larger diameter than the previous shim, and the shims may nest. The shims may comprise a thermally stable material, and the discrete spacers may comprise an elastomer. Optionally, an annular bearing protector may separate the annular shims from the flexible bearing.
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Garbe, Duane J.. 2012-10-02. Thermal protection system and related methods. https://ntrs.nasa.gov/citations/20120016380
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