NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Micro-Electromechanical Instrument and Systems Development at the Charles Stark Draper LaboratorySeveral generations of micromechanical gyros and accelerometers have been developed at Draper. Current design effort centers on tuning-fork gyro design and pendulous accelerometer configurations. Over 200 gyros of different generations have been packaged and tested. These units have successfully performed across a temperature range of -40 to 85 degrees C, and have survived 30,000-g shock tests along all axes. Draper is currently under contract to develop an integrated micro-mechanical inertial sensor assembly (MMISA) and global positioning system (GPS) receiver configuration. The ultimate projections for size, weight, and power for an MMISA, after electronic design of the application specific integrated circuit (ASIC ) is completed, are 2 x 2 x 0.5 cm, 5 gm, and less than 1 W, respectively. This paper describes the fabrication process, the current gyro and accelerometer designs, and system configurations.
Document ID
19960054119
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Connelly, J. H.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Gilmore, J. P.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Weinberg, M. S.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Instrumentation And Photography
Accession Number
96N36365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available