A nanoscale soft-ionization membrane: a novel ionizer for ion mobility spectrometers for space applications
In this paper we focus our attention on ion mobility spectrometers (IMSs) as a potential candidate to be incorporated with SIM.
Engineering topics
Publications and source records attributed to Hartley, F..
In this paper we focus our attention on ion mobility spectrometers (IMSs) as a potential candidate to be incorporated with SIM.
This paper presents differing types of non-invasive sensing technologies, differing market sectors that have requirements for these technologies, and a mannner to commercialize these technologies.
The capacity of chemically-assisted focused ion beam (fib) etching systems to undertake direct and highly anisotropic erosion of thin and thick gold (or other high atomic number [Z])coatings on x-ray mask membranes/substrates provides new levels of precision, flexibility, simplification and rapidity in the manufacture of mask absorber patterns, allowing the fast prototyping of high aspect ratio, high-resolution masks for deep x-ray lithography.
Mass is a major driver for future spacecraft, and missions exposed to high radiation levels present even more challenge. Non-invasive pressure measurement techniques that enable the accurate determination of pressures within a propulsion system will be described and their performance reviewed.
Explore the source record for details and available documents.
The ultra-sensitive accelerometer, developed for NASA to monitor the microgravity environments of Space Shuttle, free orbitors and Space Station, needed to measure accelerations up to 10mg with an absolute accuracy of 10 nano-g (10***sup-8***g) for at least two orbits (10***sup4*** seconds)to resolve accelerations associated with orbital drag.
New developments for X-ray nanomachinging include pattern transfer onto non-planar surfaces coated with eletrodeposited resists using synchrotron radion X-rays through extremely high-resolution masks made by chemically assisted focused ion beam lithography.
This paper describes reversed engineered biological peristaltics through the insightful evolution of MEMS technology. While the emphasis on pump applications is in the miniaturization of spacecraft bus and payload, terrestrial applications are evident.
Mass is a major driver for future spacecraft and missions exposed to high radiation levels (i.e. Europa Orbiter) present even more challenge. A variety of non-invasive measurement techniques are in development that enables determination of pressures within a propulsion network.
Multi-axis compact seismometers designs that have twelve decades of dynamic range will be described. Density profilometers, precision gradiometers, gyros and vibration isolation designs and applications will be discussed.
Explore the source record for details and available documents.
Reliability and quality issues are two of the main bottlenecks choking the effective commercialization of microsystem technology.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Proximity printing using synchrotron X-ray lithography provides high resolution pattern transfer with large depth of field, low diffraction effects and no reflection from the substrate. Electro-plating of photo-resist allows deposition of thin, uniform films over geometrically complex and topographically diverse, electrically conductive surfaces.
An interface is described that supplies communications between the flight instruments and the analog input of an existing conventional recording unit for the Shuttle Space Acceleration Measurement System (SAMS), a data acquisition unit. The architecture and current implementation of an STD bus/LonTalk communication interface are described.
Using micro-machined silicon technology, an ultra-sensitive miniature accelerometer can be constructed which meets the requirements for microgravity experiments in the space environment. Such an accelerometer will have a full scale sensitivity of 10 -2 g, a resolution of 10 -8 g, low cross-axis sensitivity, and low temperature sensitivity. Mass of the device is approximately five grams and its footprint is 2 cm x 2 cm.
In this paper, we report the initial development of a single-axis bulk micromachined accelerometer. The device employs an electron tunneling tip as a position detector in a force feedback control system. Control electrodes are placed above and below the proof mass and act as electrostatic force plates. Using the force plates, the position of the proof mass relative to the tunneling tip can be controlled.