NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance of MEMS Silicon Oscillator, ASFLM1, under Wide Operating Temperature RangeOver the last few years, MEMS (Micro-Electro-Mechanical Systems) resonator-based oscillators began to be offered as commercial-off-the-shelf (COTS) parts by a few companies [1-2]. These quartz-free, miniature silicon devices could compete with the traditional crystal oscillators in providing the timing (clock function) for many digital and analog electronic circuits. They provide stable output frequency, offer great tolerance to shock and vibration, and are immune to electro-static discharge [1-2]. In addition, they are encapsulated in compact lead-free packages, cover a wide frequency range (1 MHz to 125 MHz), and are specified, depending on the grade, for extended temperature operation from -40 C to +85 C. The small size of the MEMS oscillators along with their reliability and thermal stability make them candidates for use in space exploration missions. Limited data, however, exist on the performance and reliability of these devices under operation in applications where extreme temperatures or thermal cycling swings, which are typical of space missions, are encountered. This report presents the results of the work obtained on the evaluation of an ABRACON Corporation MEMS silicon oscillator chip, type ASFLM1, under extreme temperatures.
Document ID
20090004675
Document Type
Other
Authors
Patterson, Richard L. (NASA Glenn Research Center Cleveland, OH, United States)
Hammoud, Ahmad (ASRC Aerospace Corp. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Electronics and Electrical Engineering
Report/Patent Number
E-16847
Funding Number(s)
WBS: WBS 939904.11.03.01
CONTRACT_GRANT: NNC06BA07B
Distribution Limits
Public
Copyright
Public Use Permitted.

Available Downloads

NameType 20090004675.pdf STI