TURBINE ASSEMBLY

HEAT SHIELD WITH RECESSED DUAL-EXPANSION NOZZLE, AND VEHICLE INCLUDING THE SAME

High Temperature Thermal Protection System for Rockets, and Associated Methods

Augmented Aerospike Nozzle, Engine Including the Augmented Aerospike Nozzle, and Vehicle Including the Engine

COMPOSITE TUBULAR STRUCTURE

WARM GAS THRUSTER SYSTEM WITH CONTROL VALVE THAT HAS A SOFT SEAL

NOZZLE COOLING DEVICE OF A ROCKET ENGINE AND A REGENERATIVE COOLING SYSTEM OF A HYBRID ROCKET ENGINE

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

TRANSPIRATION-COOLED SYSTEMS HAVING PERMEABLE AND NON-PERMEABLE PORTIONS

THRUST VECTOR CONTROL FOR HYBRID PROPELLANTS ROCKET ENGINE WITH EMBEDDED FLUID INJECTION PORTS

REUSABLE UPPER STAGE ROCKET

Transpiration-cooled systems having permeable and non-permeable portions

Transpiration-cooled systems having permeable and non-permeable portions

Augmented aerospike nozzle, engine including the augmented aerospike nozzle, and vehicle including the engine

Combustor including heat exchange structure and rocket comprising same

ROCKET ENGINE WITH POROUS STRUCTURE

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Integrated propulsion system for hybrid rockets

Multi-part fluid chamber and method of manufacturing

Detonation rocket engine comprising an aerospike nozzle and centring elements with cooling channels

Combustor for rocket engine and method for manufacturing it

Combustor for rocket engine

Jet nozzle equipped with a thermally regulated ring

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Rocket combustion chamber wall having cooling channels and method for making thereof

Liquid-cooled air-breathing rocket engine

High temperature thermal protection system for rockets, and associated methods

Combustion chamber section with integral baffle and method of making a combustion chamber section

Upper stage rocket including aerospike nozzle defining actively-cooled re-entry heat shield

CHILLDOWN DEVICE AND METHOD

Air-Breathing rocket engine

Rocket engine with integrated oxidizer catalyst in manifold and injector assembly

Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber

Advanced Automated Fabrication System And Methods For Thermal And Mechanical Components Utilizing Quadratic Or Squared Hybrid Direct Laser Sintering, Direct Metal Laser Sintering, CNC, Thermal Spraying, Direct Metal Deposition And Frictional Stir Welding. Cross-reference To Related Applications

Thrust vector control for hybrid propellants rocket engine with embedded fluid injection ports

Rocket engine's thrust chamber assembly

Combustion chamber structure, particularly for a rocket engine

Methane/oxygen rocket engine with specific impulse enhancement by hot helium infusion

Nozzle wall for an air-breathing engine of a vehicle and method therefor

High temperature thermal protection system for rockets, and associated methods

Method for Fabricating Seal-Free Multi-Metallic Thrust Chamber Liner

Rocket motor with composite divergent nozzle section

Resin transfer molded rocket motor nozzle

Liquid propellant rocket engine nozzle with passive condensate cooling

Aerospace turbofan engines

DUAL-EXPANDER SHORT-LENGTH AEROSPIKE ENGINE

Combustion chamber structure, particularly for a rocket engine

Cooling mechanism of combustion chamber, rocket engine having cooling mechanism, and method of manufacturing cooling mechanism

Rocket propellant mixing and fueling systems and methods

Rocket engine

Rocket engine bipropellant supply system including an electrolyzer

COMBUSTOR OF A LIQUID PROPELLENT MOTOR

Propulsion chamber with reinforcing fiber belts and a method of fabricating the propulsion chamber

Divergent flap

Device for pressurizing propellant tanks of a rocket engine

Propellant feed circuit and a cooling method

Method and a device for feeding a rocket engine

Slotted multi-nozzle grid with integrated cooling channels

Engine for use in an aerial vehicle

Aircraft/spacecraft fluid cooling system and aircraft/spacecraft fluid cooling method

Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold

Combustion chamber provided with a tubular element

Multi-channel cooling plenum

Cooling device for cooling combustion gases from recoilless anti-tank weapons

Reversible flow discharge orifice

Rocket engine with cryogenic propellants

Rocket engine with cryogenic propellants

SYSTEMS, METHODS AND APPARATUS FOR PROPULSION

System, method and apparatus for cooling rocket motor components using a saturated liquid vapor coolant mixture

Method for Manufacturing a Regeneratively Cooled Nozzle Extension of a Rocket Combustion Chamber and Nozzle Extension

Method and apparatus for simplified thrust chamber configurations

Expander cycle rocket engine nozzle

COMPONENT CONFIGURED FOR BEING SUBJECTED TO HIGH THERMAL LOAD DURING OPERATION

Liner for a turbine section, a turbine section, a gas turbine engine and an aeroplane provided therewith

Fuel-cooled flexible heat exchanger with thermoelectric device compression

WALL OF A ROCKET ENGINE

Regeneratively cooled porous media jacket

ENGINE WALL STRUCTURE AND A METHOD OF PRODUCING AN ENGINE WALL STRUCTURE

Hot Gas Chamber

Method of manufacturing a wall structure and a machining tool

Device and a method for applying a coating on a workpiece by electrodeposition

Component configured for being subjected to high thermal load during operation

Carbon-Kevlar uni-body rocket engine and method of making same

Gas-generator augmented expander cycle rocket engine

SIMPLIFIED THRUST CHAMBER RECIRCULATING COOLING SYSTEM

Rocket nozzle and control method for combustion gas flow in rocket engine

Reinforced, regeneratively cooled uni-body rocket engine

Heat exchanger for a rocket engine

Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct

Method of fabricating a rocket engine nozzle using pressure brazing

Engine wall structure and a method of producing an engine wall structure

Method of producing an engine wall structure

Systems, methods and apparatus for propulsion

Rocket engine combustion chamber

System and method for cooling hydrocarbon-fueled rocket engines

Gas augmented rocket engine

Outlet nozzle and a method for manufacturing an outlet nozzle

Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing

Rocket engine chamber with layered internal wall channels

Component for being subjected to high thermal load during operation and a method for manufacturing such a component

Advanced L-channel welded nozzle design

System and fabrication method for actively cooling high performance components

Method of assembling a rocket engine with a transition zone between the combustion chamber and the coolant system

Method of manufacturing an active cooling panel out of thermostructural composite material

Transpiration cooling system

Composite tubular structure

Heavy inert gas insulated blast tube

Afterburning turbine exhaust cycle (ABTEC)

Dual mode rocket engine with bipropellant injection in the nozzle

Liquid rocket engine cooling channels

Rocket engine injector

Liquid-cooled air-breathing rocket engine

Liquid rocket engine cooling channels

Liquid rocket engine cross impinged propellant injection

Thermoelectric rocket propellant tank pressurization system

Cladding and freeform deposition for coolant channel closeout

Freeform deposition method for coolant channel closeout

Rocket engine thrust chamber, injector, and turbopump