Development and Characterization of Inductively Heated Plasma Generators for Atmospheric Entry Simulations-Reference-Cited by-同舟云学术

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Development and Characterization of Inductively Heated Plasma Generators for Atmospheric Entry Simulations

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Herdrich Georg¹,Auweter-Kurtz Monika¹

Affiliation:

1. University of Stuttgart

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2503

Reference33 articles.

1. [4]Curry, D.M., Space Shuttle Orbiter Thermal Protection System Design and Flight Experience, NASA Technical Memorandum104773, July1993.

2. Oxidation of Hypervelocity Impacted Reinforced Carbon-Carbon

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2. Aerothermodynamic Investigation of Inductively Heated CO2 Plasma Flows for Mars Entry Testing;45th AIAA Plasmadynamics and Lasers Conference;2014-06-13

3. Enthalpy Distributions of Laser Driven High Enthalpy Wind Tunnel;26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2008-06-15

4. Enthalpy Measurement of Inductively Heated Airflow;Journal of Spacecraft and Rockets;2008-01

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