Deployment and retrieval mechanism redesigned for Spartan spacecraft on the STS

Greg Galloway

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NASA NTRS · 19920015828

Deployment and retrieval mechanism redesigned for Spartan spacecraft on the STS

Greg Galloway

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Abstract

The Spartan Release Engage Mechanism (REM) is a system designed to restrain the Spartan spacecraft during Space Transportation System (STS) launch and landing. The mechanism is designed to allow deployment and retrieval of the Spartan free flyer spacecraft from the shuttle payload bay. Because current Spartan spacecraft payloads are much heavier than payloads intended for the original REM, an extensive redesign, analysis, and test program was necessary. Also, increased emphasis on safety in the post-Challenger era prompted a reevaluation of possible failures. Much of the design effort focused on improving the latch mechanism gearbox. Key concerns were effective gear lubrication, thermal gradients at the gearbox mounts, operation at thermal extremes, and gear-train failure contingencies. Increased concern for reliability led to the design of an Extra Vehicular Activity (EVA) backup latch system.

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Greg Galloway. 1992-05-01. Deployment and retrieval mechanism redesigned for Spartan spacecraft on the STS. https://ntrs.nasa.gov/citations/19920015828

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