NASA NTRS · 19880004248
High frequency data acquisition system for space shuttle main engine testing
Abstract
The high frequency data acquisition system developed for the Space Shuttle Main Engine (SSME) single engine test facility at the National Space Technology Laboratories is discussed. The real time system will provide engineering data for a complete set of SSME instrumentation (approx. 100 measurements) within 4 hours following engine cutoff, a decrease of over 48 hours from the previous analog tape based system.
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Lewallen, Pat. 1987-10-01. High frequency data acquisition system for space shuttle main engine testing. https://ntrs.nasa.gov/citations/19880004248
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