Synthesis and Characterization of Hyperbranched Polyazomethine Ablators for Space Exploration Applications-Reference-Cited by-同舟云学术

Synthesis and Characterization of Hyperbranched Polyazomethine Ablators for Space Exploration Applications

Published:2014-07 Issue:3 Volume:28 Page:401-409
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Tigelaar Dean M.¹,Degges Matthew J.²,Chuang Kathy¹,Hurwitz Frances I.³,Kuo Kenneth K.²,Scheiman Daniel A.⁴,McCorkle Linda S.⁴,Quade Derek J.⁴,Vivod Stephanie L.⁴,Splinter Scott⁵

Affiliation:

1. Polymers Branch, NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135

2. Department of Mechanical and Nuclear Engineering, Pennsylvania State University, State College, Pennsylvania 16801

3. Structure and Materials Division, NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135

4. ASRC, NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135

5. Structural Mechanics and Concepts Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.T4319

Reference22 articles.

1. WilsonR.KoubekF. “High Viscosity Thermal Protection Materials,” NOL TR-68-216, 1969.

2. Polymers for potential use as charring ablators under hyperthermal re-entry conditions: A review of recent developments

3. Ablative Polymers in Aerospace Technology

4. Analytical and Kinetic Modeling of Ablation Process

5. Numerical Modeling of Ablation Heat Transfer

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