The construction of detailed computational models of the dynamic behavior of various explosive ordnance devices used on space vehicles is discussed. The following topics are presented in viewgraph form: numerical methods, explosives and detonations, and the MESA computer code.
Application of the MESA Reactive Hydrocode to Space Vehicle Explosive Ordnance Devices
1993
36 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Ammunition, Explosives, & Pyrotechnics , Space Safety , Applications programs (Computers) , Detonation , Explosive devices , Hydrodynamics , Impact tests , Ordnance , Three dimensional models , Two dimensional models , Dynamic characteristics , Explosives , Finite difference theory , Mathematical models , Numerical analysis , Partial differential equations , Solid propellant ignition , Aerospace safety
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