Determination of thermal performance of char under heating conditions simulating atmospheric entry
Author:
Affiliation:
1. GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., RE-ENTRY SYSTEMS DEPT., PHILADELPHIA, PA.
2. GENERAL ELECTRIC CO., ATOMIC PRODUCTS DIV., CINCINNATI, OHIO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1965-640
Reference3 articles.
1. Physical Review, V. 86, No. 2, April 15, 1952.
2. Sept. 30 - Ocf. 1, 1963, Lockheed Missiles and Space Company. 3. Brazel, 3. P."Transient Determination of The Thermal CodnctiviFj of A Lau
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Thermal Physical Characteristics of High-Performance Ablative Composites;Journal of Macromolecular Science: Part A - Chemistry;1969-07
2. Mechanical erosion of charring ablators in ground-test and re-entry environments.;AIAA Journal;1968-01
3. SNAP 10A THERMAL CONTROL COATINGS;Thermophysics and Temperature Control of Spacecraft and Entry Vehicles;1966
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