Abstract: An air intake for an aircraft propulsion system includes a cowl including a longitudinal axis. The air intake includes a compression ramp spaced away from the cowl. The air intake includes an inlet duct formed between the cowl and the compression ramp. The inlet duct defines an inlet airflow path. The compression ramp is non-planar. The compression ramp is movable relative to the cowl to vary compression of the inlet airflow passing through the inlet duct.

Abstract: A propulsion system for an aircraft includes an engine having a central axis. A cowl surrounds the engine and includes a cowl lip. A compression ramp is spaced away from the cowl lip. An inlet is formed by the cowl lip and the compression ramp. The compression ramp is non-planar. The compression ramp is movable relative to the cowl lip to vary compression of an inlet airflow through the inlet.

Abstract: A propulsion system for an aircraft includes an engine having a central axis. A cowl surrounds the engine and includes a cowl lip. A compression ramp is spaced away from the cowl lip. An inlet is formed by the cowl lip and the compression ramp. The compression ramp is non-planar. The compression ramp is movable relative to the cowl lip to vary compression of an inlet airflow through the inlet.

Abstract: Systems and methods for expanding an operating speed range of a high speed flight vehicle include providing an engine with an inlet air duct, and positioning a heat exchanger in the inlet air duct to cool at least a portion of duct air flow associated with an engine core. Additionally or alternatively, a nozzle assembly includes a cowl fluidly communicating with the engine and having a cowl internal surface defining a cowl orifice, and a plug defines a primary thrust surface. The plug is supported relative to the cowl so that a portion of the primary thrust surface is disposed within the cowl orifice to define a throat therebetween. An actuator is coupled to at least one of the cowl or the plug, and is configured to generate relative movement between the cowl and the plug, thereby to modify the throat.

Abstract: A gas delivery system and method for delivering reactants such as a first gas through a first conduit and a second gas through at least one second conduit, for example, through a plurality of second conduits. The plurality of second conduits may each have a length, wherein at least a portion of the length is entirely disposed within the first conduit. In an implementation, the first conduit may deliver carbon monoxide and the one or more second conduits may deliver carbon monoxide doped with a catalyst such as iron pentacarbonyl. The first and second gases may be introduced into a reaction vessel such as a reactor chamber and used to form carbon nanotubes.

Abstract: A gas delivery system and method for delivering reactants such as a first gas through a first conduit and a second gas through at least one second conduit, for example, through a plurality of second conduits. The plurality of second conduits may each have a length, wherein at least a portion of the length is entirely disposed within the first conduit. In an implementation, the first conduit may deliver carbon monoxide and the one or more second conduits may deliver carbon monoxide doped with a catalyst such as iron pentacarbonyl. The first and second gases may be introduced into a reaction vessel such as a reactor chamber and used to form carbon nanotubes.

Abstract: A gas delivery system and method for delivering reactants such as a first gas through a first conduit and a second gas through at least one second conduit, for example, through a plurality of second conduits. The plurality of second conduits may each have a length, wherein at least a portion of the length is entirely disposed within the first conduit. In an implementation, the first conduit may deliver carbon monoxide and the one or more second conduits may deliver carbon monoxide doped with a catalyst such as iron pentacarbonyl. The first and second gases may be introduced into a reaction vessel such as a reactor chamber and used to form carbon nanotubes.

Abstract: A gas delivery system and method for delivering reactants such as a first gas through a first conduit and a second gas through at least one second conduit, for example, through a plurality of second conduits. The plurality of second conduits may each have a length, wherein at least a portion of the length is entirely disposed within the first conduit. In an implementation, the first conduit may deliver carbon monoxide and the one or more second conduits may deliver carbon monoxide doped with a catalyst such as iron pentacarbonyl. The first and second gases may be introduced into a reaction vessel such as a reactor chamber and used to form carbon nanotubes.