Hostname: page-component-74656f9884-8r8nv Total loading time: 0 Render date: 2026-11-07T13:23:19.041Z Has data issue: false hasContentIssue false

Nanoelectronics and nanosensors for space exploration

Published online by Cambridge University Press:  08 October 2015

M. Meyyappan
Affiliation:
NASA Ames Research Center, USA; m.meyyappan@nasa.gov
Jessica E. Koehne
Affiliation:
NASA Ames Research Center, USA; jessica.e.koehne@nasa.gov
Jin-Woo Han
Affiliation:
NASA Ames Research Center, USA; jin-woo.han@nasa.gov

Abstract

Space missions have unique requirements for payloads of electronics, sensors, instruments, and other components in terms of mass, footprint, power consumption, and resistance to various types of radiation. Nanomaterials offer the potential for future radiation-hardened or radiation-immune electronics. Gas-sensing needs in planetary exploration and crew-cabin air-quality monitoring are currently being met by bulky instruments. Routine health checkups of astronauts and testing of water in space habitats are being done on a delayed basis by bringing samples back to Earth. Instead, nanomaterials can be used to construct ultrasmall, postage-stamp-sized gas/vapor sensors with selective discrimination and also lab-on-a-chip biosensors for water-quality monitoring and crew health monitoring.

Information

Type
Research Article
Copyright
Copyright © Materials Research Society 2015 
Figure 0

Figure 1. Phase-change random-access memory. (a) Conventional thin-film-based memory cell and (b) nanowire-based memory device. The top electrode is in red, and the bottom electrode is in orange. The light blue region represents the phase-change material, and the dark blue region denotes the portion undergoing the phase change. The bottom electrode in (a) is surrounded by oxide (striped).

Figure 1

Figure 2. (a) Silicon-based nanoscale vacuum transistor with a bottom gate. (b) The highly doped source and drain electrodes (E and C) with a specified gap are created by plasma ashing, as shown in the scanning electron microscope image.

Figure 2

Figure 3. (a) Nanoelectrode array using vertical carbon nanofibers. The exposed tips of the carbon nanofibers are seen as white dots. (b) Differential pulse voltammetry results for the detection of target myoglobin. Blue, bare electrode; red, after antibody immobilization; green, after introduction of myoglobin target protein. Note: SCE, saturated calomel electrode.

Figure 3

Figure 4. (a) Image of a gas sensor array (1.7 cm × 2.0 cm) fabricated on a printed circuit board. S01–S16 indicates the individual sensors. (b) Responses of various sensors in the array to successive exposures to 2, 10, 25, 50, 75, and 100 ppm of CO. The inset shows the response versus concentration calibration curve. Images courtesy of Yijiang Lu and Ami Hannon, NASA Ames Research Center, Mountain View, Calif.