NASA NTRS · 19760034960
ATS-6 - Flight accelerometers
Abstract
The Applications Technology Satellite-6 (ATS-6) flight accelerometers were designed to provide data for verifying the basic spacecraft vibration modes during launch, to update the analytical model of the ATA structure, and to provide a capability for detection and diagnosis of inflight and anomalies. The experiment showed accelerations less than 2.5 g during liftoff and 1.1 g or less during staging with frequencies below 80 Hz. Measured values were generally within 1 g of predicted.
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Mattson, R., Honeycutt, G., Lindner, F.. 1975-11-01. ATS-6 - Flight accelerometers. https://ntrs.nasa.gov/citations/19760034960
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