140465 ⎘
Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof; Rocket nozzles Nozzle- linings; Ablative coatings
High Temperature Thermal Protection System for Rockets, and Associated Methods
#2EVANESCENT OR FUGACIOUS THRUST DEFLECTOR
#3HIGH-TEMPERATURE ABLATION RESISTANT HIGH-ENTROPY ALLOY FOR THROAT LINER AND MANUFACTURING METHOD THEREFOR
#4COATING SYSTEM FOR REFRACTORY METALS
#5RESIN FORMULATIONS AND RELATED ARTICLES AND METHODS
#6EVANESCENT OR FUGACIOUS THRUST DEFLECTOR
#7Thermal protection device for a nozzle
#8High temperature thermal protection system for rockets, and associated methods
#9Impregnated fibers comprising preceramic resin formulations, and related composite materials and methods
#10DYNAMIC ROCKET NOZZLE
#11Ceramic materials comprising preceramic resin formulations, and related articles and methods
#12Resin transfer molded rocket motor nozzle with adaptive geometry
#13Barrier coating resin formulations, and related methods
#14High temperature thermal protection system for rockets, and associated methods
#15Method for Fabricating Seal-Free Multi-Metallic Thrust Chamber Liner
#16Resin transfer molded rocket motor nozzle
#17Manufacturing process for making a dome element provided with thermal protection for a solid propellant rocket engine
#18THRUSTER WITH COMBUSTION CHAMBER AND NOZZLE USING HONEYCOMB STRUCTURE
#19Ceramic matrix composite articles
#20COATING SYSTEM FOR REFRACTORY METALS
#21Preceramic resin formulations, ceramic materials comprising the preceramic resin formulations,and related articles and methods
#22Preceramic resin formulations, impregnated fibers comprising the preceramic resin formulations, and related methods
#23Fragmenting nozzle system
#24Panel surface pockets for coating retention
#25Fragmenting nozzle system
#26Space storable, thrust-vectorable rocket motor nozzle and related methods
#27Lightning protection device and method of producing same
#28Combustion chamber provided with a tubular element
#29Rocket multi-nozzle grid assembly and methods for maintaining pressure and thrust profiles with the same
#30Combustion chamber comprising a condensation-proof barrier on a regenerative circuit
#31SYSTEMS, METHODS AND APPARATUS FOR PROPULSION
#32Process for producing a self-healing layer on a part made of a C/C composite
#33Jet vane and method for manufacturing a jet vane
#34Rocket motors incorporating basalt fiber and nanoclay compositions and methods of insulating a rocket motor with the same
#35METHOD FOR FORMING AN OXIDATION-RESISTANT FILM
#36Method for fabricating a component having an environmental barrier coating
#37Environmental barrier coating for a component and method for fabricating the same
#38Heat exchanger for a rocket engine
#39Thermal barrier coating member, method for producing the same, thermal barrier coating material, gas turbine, and sintered body
#40PROCESS FOR THE REPAIR AND RESTORATION OF DYNAMICALLY STRESSED COMPONENTS COMPRISING ALUMINIUM ALLOYS FOR AIRCRAFT APPLICATIONS
#41LOW COST, LOW-DENSITY, ABLATIVE RUBBER INSULATION FOR ROCKET MOTORS
#42Combustible outgassing material lined altitude compensating rocket nozzle
#43Structural element and method for producing the same
#44Systems, methods and apparatus for propulsion
#45Variable area flow duct employing secondary flows, and method therefor
#46Rocket engine combustion chamber
#47Basalt fiber and nanoclay compositions, articles incorporating the same, and methods of insulating a rocket motor with the same
#48Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine
#49Liquid propellant rocket engine with pintle injector and acoustic dampening
#50Rocket nozzle material
#51Use of controlled atmosphere plasma spray combined with electrodeposition to fabricate a rocket engine chamber
#52Throat retention apparatus for hot gas applications
#53Extremely strain tolerant thermal protection coating and related method and apparatus thereof
#54Ablative afterburner
#55Method of assembling a rocket engine with a transition zone between the combustion chamber and the coolant system
#56Method of manufacturing an active cooling panel out of thermostructural composite material
#57Ablative composite assemblies and joining methods thereof
#58Method of insulating a case of a solid propellant rocket motor
#59Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same
#60Heavy inert gas insulated blast tube
#61Self compensating rocket engine enhancement