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RAKETENANTRIEB
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keywords:(RAKETENANTRIEB)
Mechanische Integrität von Wärmedämmschichten für den Einsatz in Raketenbrennkammern
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Hybrid Carbon-Carbon Ablative Composites for Thermal Protection in Aerospace
High Temperature, High Performance Materials for Liquid Rocket Engines
High temperature, high performance materials for liquid rocket engines
Novel Techniques for Ceramic Composite Processing
Nanocrystalline Materials: A Critical Review
Advanced Composite Materials for Rocket Engines and Space Applications
Tensile Deformation of Titanium-Tantalum Alloys
Dynamic Simulation of Insulation Material Ablation Process in Solid Propellant Rocket Motor
High Temperature Applications of Ceramic Matrix Composites
Composites in High Speed Turbines for Rocket Engines
Composites in high speed turbines for rocket engines
GlidCop[R] Dispersion Strengthened Copper Plus Niobium-An Advanced Composite Material
Nickel Aluminide(Ni~3Al) Fabricated by Reactive Infiltration
The Deposition of Silica on Carbon as a Model System for Oxidation Protection Coatings
Development of an acoustic emission strand burning technique for motor burning rate prediction