Nuclear radiation effects on the ablation performance of advanced composite heatshield materials

Author:

WENGER R.1,LAGANELLI A.1,SOMERS J.2

Affiliation:

1. Science Applications, Inc., El Segundo, CA

2. U.S. Defense Nuclear Agency, Washington, DC

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Effects of improvements and uncertainties in thermophysical properties on carbon phenolic heatshield thermal performance predictions

2. Suchsland. K.E. and Maurer. R.E. "A Unified Ablative 'Material Thermal Respoise Analysis Procedure," A i r Force Materials Laboratory Report AFML-TR-76-46, Contract F33615-74-C5030, April 1976

Cited by 4 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. Development of Heat Conduction Analysis Model Considering Thermal Expansion of Ablator;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022

2. Development of Lightweight Ablator Using Porous Carbon Material;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2016

3. Application of integral methods to ablation charring erosion - A review;Journal of Spacecraft and Rockets;1995-03

4. Hybrid integral/quasi-steady solution of charring ablation;5th Joint Thermophysics and Heat Transfer Conference;1990-06-18

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