NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
ATS-6 - Flight accelerometersThe 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.
Document ID
19760034960
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mattson, R. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Honeycutt, G. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Lindner, F. (NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-11
Subject Category
Spacecraft Instrumentation
Accession Number
76A17926
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available