Analysis of a transpiration cooled LOX/CH<mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" altimg="si9.svg"><mml:msub><mml:mrow/><mml:mn>4</mml:mn></mml:msub></mml:math> rocket thrust chamber
David J. Munk, Markus Selzer, Helge Seiler, Markus Ortelt, Gareth A. Vio
Topics & Concepts
TranspirationThrustCeramicRocket (weapon)Materials scienceMechanical engineeringNuclear engineeringComputer scienceAerospace engineeringThermodynamicsPhysicsChemistryComposite materialEngineeringPhotosynthesisBiochemistryRocket and propulsion systems researchHeat transfer and supercritical fluidsGas Dynamics and Kinetic Theory