Add to ORKGA combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel delivery system aft of the axial fuel delivery system. The radial fuel delivery system may be configured to direct fuel at least partially towards the axial fuel delivery system. A radial fuel delivery system is also provided. The system may comprise a combustor including a combustor liner, a mixer coupled to the combustor liner, and a nozzle disposed within the mixer, wherein the mixer and the nozzle are configured to direct fuel in a direction at least partially forward
KSC Processing Configuration and Data Report is being provided as a historical document and as an en...
The emissions performance of a rich lean combustor (developed for liquid fuels) for combustion of si...
This system architecture task (1) analyzed the current process used to make an assessment of engine ...
Exemplary deployable sheet material systems may be configured to stow and deploy sheet material. The...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
Described herein are composites that are relatively lightweight, high strength and low thermal condu...
Ion optics for use in a conventional or annular or other shaped ion thruster are disclosed including...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silico...
Recent advances in commercial and military aircraft gas turbines have yielded significant improvemen...
About fifty industrial processes from the largest energy consuming sectors were used as a basis for ...
An actuator includes a housing assembly, a ball nut, a ball screw, and a ball screw stop. The ball n...
A power generation system includes a plurality of submerged mechanical devices. Each device includes...
A functional design of a rotorcraft digital advanced avionics system (RODAAS) to transfer the techno...
KSC Processing Configuration and Data Report is being provided as a historical document and as an en...
The emissions performance of a rich lean combustor (developed for liquid fuels) for combustion of si...
This system architecture task (1) analyzed the current process used to make an assessment of engine ...
Exemplary deployable sheet material systems may be configured to stow and deploy sheet material. The...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
Described herein are composites that are relatively lightweight, high strength and low thermal condu...
Ion optics for use in a conventional or annular or other shaped ion thruster are disclosed including...
A combustor assembly includes a first wall, a second wall, a bulkhead and a plurality of fuel inject...
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silico...
Recent advances in commercial and military aircraft gas turbines have yielded significant improvemen...
About fifty industrial processes from the largest energy consuming sectors were used as a basis for ...
An actuator includes a housing assembly, a ball nut, a ball screw, and a ball screw stop. The ball n...
A power generation system includes a plurality of submerged mechanical devices. Each device includes...
A functional design of a rotorcraft digital advanced avionics system (RODAAS) to transfer the techno...
KSC Processing Configuration and Data Report is being provided as a historical document and as an en...
The emissions performance of a rich lean combustor (developed for liquid fuels) for combustion of si...
This system architecture task (1) analyzed the current process used to make an assessment of engine ...