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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 145 records · Page 8

Reliability Issues of COTS MEMS Packaging

During the last decade, research and development of microelectromechanical systems (MEMS) has shown a significant promise for a variety of commercial applications including automobile and medical purposes.

Microelectromechanical systems MEMS reliability IC↗

MEMS for Space Flight Applications

Micro-Electrical Mechanical Systems (MEMS) are entering the stage of design and verification to demonstrate the utility of the technology for a wide range of applications including sensors and actuators for military, space, medical, industrial, consumer, automotive and instrumentation products.

AFM infrared microscopy IR light emission microsco↗

A Packaged Silicon MEMS Vibratory Gyroscope for Microspacecraft

In this paper, we present recent work on the design, fabrication, and packaging of a silicon MIcro-Electro-Mechanical System (MEMS) microgyroscope designed for space applications. A hermetically sealed package that houses the microgyroscope and most of its control electronics has been built and tested.

MEMS micro-electromechanical system microspacecraf↗

MEMS based sun sensor on a chip

A prototype sun sensor has been developed. The accuracy of the MEMS based sun sensor on a chip is estimated to be 1 arcminute.

MEMS sun sensor APS attitude determination↗

An overview of MEMS-based micropropulsion development at JPL

Development of MEMS (Microelectromechanical Systems) micropropulsion at the Jet Propulsion Laboratory (JPL) is reviewed. This includes a vaporizing liquid micro-thruster for microspacecraft attitude control, a micro-ion emgine for microspacecraft primary propulsion or large spacecraft fine attitude control, as well as several valve studies, including a solenoid valve studied in collaboration with Moog Space Products Division, and a piezoelectric micro-valve.

MEMS micropropulsion↗

MEMS AO for Planet Finding

This slide presentation reviews a method for planet finding using microelectromechanical systems (MEMS) Adaptive Optics (AO). The use of a deformable mirror (DM) is described as a part of the instrument that was designed with a nulling interferometer. The strategy that is used is described in detail.

calibration interferometer↗

Path Length Control in a Nulling Coronagraph with a MEMS Deformable Mirror and a Calibration Interferometer

We report progress on a nulling coronagraph intended for direct imaging of extrasolar planets. White light is suppressed in an interferometer, and phase errors are measured by a second interferometer. A 1020-pixel MEMS deformable mirror in the first interferometer adjusts the path length across the pupil. A feedback control system reduces deflections of the deformable mirror to order of 1 nm rms.

MEMS adaptive optics↗

Single Event Effect Testing of the Analog Devices ADXL354 3-Axis MEMS Accelerometer

The Analog Devices ADXL354 3-AXIS MEMS accelerometer was tested for single-event effects, both destructive and non-destructive. The device was characterized for single-event upset (SEU) sensitivity and evaluated for any possibility of single-event latchup (SEL), single-event dielectric rupture (SEDR) and single-event functional interrupts (SEFI). Single-event transient (SET) response was also monitored.

Single-Event Effect (SEE)↗

MEMS for Space Applications

The future of robotic space missions in ever-smaller platforms and MicroElectroMechanical Systems (MEMS) will be key in this development.

MEMS↗