Methodology for Flight-Relevant Arc-Jet Testing of Flexible Thermal Protection Systems-Reference-Cited by-同舟云学术

Methodology for Flight-Relevant Arc-Jet Testing of Flexible Thermal Protection Systems

Published:2014-05 Issue:3 Volume:51 Page:789-800
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Mazaheri Alireza¹,Bruce Walter E.¹,Mesick Nathaniel J.²,Sutton Kenneth³

Affiliation:

1. Aerothermodynamics Branch, NASA Langley Research Center, Hampton, Virginia 23681

2. Mechanical Systems Branch, Science System and Applications, Inc., Hampton, Virginia 23666

3. Aerothermodynamics Branch, National Institute of Aerospace, Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32721

Reference15 articles.

1. Advanced High-Temperature Flexible TPS for Inflatable Aerodynamic Decelerators

2. “Evaluation of the NASA Arc-Jet Capabilities to Support Mission Requirements,” NASA SP-2010-577, May 2010.

3. ZobyV. “Effects of Corner Radius on Stagnation-Point Velocity Gradients on Blunt Axisymmetric Bodies,” NASA TM-X-1067, 1964.

4. SuttonK.GravesR. A.Jr. “A General Stagnation-Point Convective Heating Equation for Arbitrary Gas Mixtures,” NASA TR-376, 1971.

5. GuptaR.YosJ.ThompsonR. A.LeeK. “A Review of Reaction Rates and Thermodynamic and Transport Properties for an 11-Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30,000 K,” NASA RP-1232, 1990.

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