A triaxial piezoelectric accelerometer was developed, fabricated, tested and calibrated for use in the NASA Get-Away-Special (GAS) to be flown on the space shuttle vehicle. It is to be used for the determination of the low-level vibration environment of the instrument pallet during orbital operation, and for the possible measurement of orbital drag deceleration. (Author)
Micro-g Triaxial Piezoelectric Satellite Accelerometer System Development
1981
45 pages
Report
No indication
English