NASA NTRS · 19700062424
Development and testing of a triaxial angular accelerometer for high-performance aerospace vehicles
Abstract
Seismic fluid suspended triaxial angular accelerometer for high performance aerospace vehicle flight test application
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Evans, R. D., Jr.. 1970-01-01. Development and testing of a triaxial angular accelerometer for high-performance aerospace vehicles. https://ntrs.nasa.gov/citations/19700062424
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