The heat protection potential of several ablation materials for satellite and ballistic re-entry into the earth's atmosphere-Reference-Cited by-同舟云学术

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The heat protection potential of several ablation materials for satellite and ballistic re-entry into the earth's atmosphere

Published:1961-01 Issue: Volume:4 Page:463-478
ISSN:0032-0633
Container-title:Planetary and Space Science
language:en
Short-container-title:Planetary and Space Science

Author:

Diaconis N.S.,Fanucci J.B.,Sutton G.W.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference20 articles.

1. The Mechanism of Polytetrafluorethylene Pyrolysis;Friedman,1959

2. Compressible Couette Flow with Diffusion of a Reactive Gas from a Decomposing Wall;Knuth,1958

3. Combustion of a Gas Injected into a Hypersonic Laminar Boundary Layer;Sutton,1958

4. The Thermal Protection of a Re-entry Satellite;Scala,1959

Cited by 5 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. Pyrolysis of Phenolic Impregnated Carbon Ablator (PICA);ACS Applied Materials & Interfaces;2014-12-22

2. The Ablation of Slip-Cast Fused Silica;Journal of Spacecraft and Rockets;1972-03

3. A method of calculating teflon mass removal when teflon is broken up in a high temperature gas flow;Journal of Engineering Physics;1971-01

4. Evaluation methods for ablative plastics. A review of the techniques used;Polymer Engineering and Science;1963-10

5. Determination of the Shock Pressure Required to Initiate Detonation of an Acceptor in the Shock Sensitivity Test;ARS Journal;1962-01

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