Hypervelocity impacts of orbital debris on an advanced heat shielding material: comparison of ouranos computations to experimental results

Author:

Loupias C.,Sibeaud J.M.,Hereil P.L.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference9 articles.

1. Description of a 20 mm caliber double-stage light gas gun with a new sabot/projectile separation technique;Loupias,1994

2. Logiciel OURANOS : présentation et utilisation en détonique;Jourdren;Revue Scientifique et Technique de la Défense,1995

3. The effect of projectile properties on target cratering;Williams;Int. J. Impact Engng.,1987

4. Effects of parametric variations of complex targets on damage from projectile impact;Meir;Int. J. Impact Engng.,1990

5. Explosive simulation to investigate enhanced ablator removal;Sanai;Int. J. Impact Engng.,1993

Cited by 2 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. Orbital debris impact damage to reusable launch vehicles;International Journal of Impact Engineering;1999-12

2. Development of material models for Nextel and Kevlar-epoxy for high pressures and strain rates;International Journal of Impact Engineering;1999-12

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