Characterization of a Large-Scale Arcjet Facility Using Tunable Diode Laser Absorption Spectroscopy
Author:
Affiliation:
1. AMA, Inc., Moffett Field, California 94045
2. NASA Ames Research Center, Moffett Field, California 94035
Funder
Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056011
Reference21 articles.
1. Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles
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3. High Enthalpy Test Methodologies for Thermal Protection Systems Development at NASA Ames Research Center
4. A survey of current and future plasma arc-heated test facilities for aerospace and commercial applications
5. KimS. “Development of Tunable Diode Laser Absorption Sensors for a Large-Scale Arc-Heated-Plasma Wind Tunnel,” Ph.D. Dissertation, Stanford Univ, Stanford, CA, 2004, http://hanson.stanford.edu/dissertations/Kim_2004.pdf [retrieved 2017].
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