Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2011.

Bibliographic Details
Main Author: Field, Ella Suzanne
Other Authors: Luis Velásquez-García.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2012
Subjects:
Online Access:http://hdl.handle.net/1721.1/68944
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author Field, Ella Suzanne
author2 Luis Velásquez-García.
author_facet Luis Velásquez-García.
Field, Ella Suzanne
author_sort Field, Ella Suzanne
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2011.
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spelling mit-1721.1/689442019-04-10T23:00:09Z Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites Field, Ella Suzanne Luis Velásquez-García. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Massachusetts Institute of Technology. Dept. of Mechanical Engineering. Mechanical Engineering. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2011. Cataloged from PDF version of thesis. Includes bibliographical references (p. 81-84). One of the most important technical goals in spacecraft design is maintaining the vehicle's integrity under the extreme conditions encountered during reentry to the Earth's atmosphere. When a hypersonic vehicle travels through the atmosphere, a high-density and low-temperature plasma sheath forms around it due to shock heating of the surrounding air and ablation of the heat shield material, which leads to the dissociation and ionization of the background atmosphere. The plasma sheath that surrounds the spacecraft affects the heat transfer to the spacecraft, its aerodynamics, and its capability to communicate. A thorough knowledge of reentry plasma sheath properties is needed to effectively develop reentry vehicles capable of maintaining structural integrity, aerodynamic stability, and communications during reentry. This thesis reports the preliminary development of a novel plasma diagnostics technology that is modular and that can be used to both monitor the reentry of a spacecraft and serve as a scientific payload in a miniaturized satellite. The technology utilizes planar arrays of batch-fabricated micro Langmuir probes that can be surface-mounted on a reentry vehicle or miniaturized satellite as a sensorial skin to perform time-resolved measurements of the electron temperature and number density of the surrounding plasma sheath. These low-cost, miniaturized plasma sensors align with the paradigm shift in space technology, where missions are visibly smaller, inexpensive, and high performance. A rough analysis of the reentry heat transfer and plasma data, and our own microfabrication capabilities, led to the design and batch-fabrication process of the micro Langmuir probes. The micro Langmuir probes were constructed by filling-in with electroless nickel 100 pm-diameter tapered vias machined into a Pyrex substrate, resulting in individually addressable probes having 600 ptm-diameter tips. The highest density arrays that were fabricated consist of 25 probes per 1 cm-square tile, having 1.6 mm separation between probes and square packing, though up to 39 probes per 1 cm-square are possible. The MEMS Langmuir probes were preliminarily tested in a plasma environment similar to atmospheric reentry at MIT's Versatile Toroidal Facility (VTF). The MEMS Langmuir probes were operated as a current-mode triple probe to obtain real-time estimates of the electron temperature, number density, and Debye length. The performance of the MEMS Langmuir probes as a triple probe was benchmarked using a homemade conventional triple Langmuir probe. The plasma parameters measured by the MEMS Langmuir probe were within the range of VTF's reported plasma parameters, but the estimates of the electron density and Debye length were not within the range of the estimates from the conventional triple Langmuir probe using identical plasma. Therefore, we believe that better driving circuitry is needed to increase the signal-to-noise ratio in the MEMS probe data. Nonetheless, these preliminary results suggest that the MEMS Langmuir probe technology has a promising role for conducting reentry plasma diagnostics and serving as nanosatellite scientific payload. by Ella Suzanne Field. S.M. 2012-01-30T17:05:01Z 2012-01-30T17:05:01Z 2011 2011 Thesis http://hdl.handle.net/1721.1/68944 773813629 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 84 p. application/pdf Massachusetts Institute of Technology
spellingShingle Mechanical Engineering.
Field, Ella Suzanne
Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title_full Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title_fullStr Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title_full_unstemmed Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title_short Batch-microfabricated miniaturized planar arrays of Langmuir probes for reentry plasma diagnostics and nanosatellites
title_sort batch microfabricated miniaturized planar arrays of langmuir probes for reentry plasma diagnostics and nanosatellites
topic Mechanical Engineering.
url http://hdl.handle.net/1721.1/68944
work_keys_str_mv AT fieldellasuzanne batchmicrofabricatedminiaturizedplanararraysoflangmuirprobesforreentryplasmadiagnosticsandnanosatellites