Modelling oblique hypervelocity impact phenomena using elementary shock physics

During their missions in space, spacecraft are subjected to high velocity impacts by orbital debris particles. Such impacts are expected to occur at non-normal incidence angles and can cause severe damage to the spacecraft as well as to its external flight-critical components. In order to ensure cre...

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Veröffentlicht in:	International journal of impact engineering 1999-12, Vol.23 (1), p.823-834
Hauptverfasser:	Schonberg, William P., Ebrahim, Ahmed R.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft industry. Spacecraft Applications Applied sciences Contact of materials. Friction. Wear Engineering techniques in metallurgy. Applications. Other aspects Exact sciences and technology Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy
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