Ion optics for use in a conventional or annular or other shaped ion thruster are disclosed including a plurality of planar, spaced apart ion optic electrode pairs sized to include a diameter smaller than the diameter of thruster exhaust and retained in, on or otherwise associated with a frame across the thruster exhaust. An electrical connection may be provided for establishing electrical connectivity among a set of first upstream electrodes and an electrical connection may be provided for establishing electrical connectivity among the second downstream electrodes
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
An aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser ...
Systems and methods for lightweight, customizable antenna with improved performance and mechanical p...
An electric propulsion machine includes an ion thruster having a discharge chamber housing a large s...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
An amorphous robot includes a compartmented bladder containing fluid, a valve assembly, and an outer...
An actuator includes a housing assembly, a ball nut, a ball screw, and a ball screw stop. The ball n...
A lower robotic arm includes a base structure, a plurality of digits, and a plurality of tendons. Th...
A power generation system includes a plurality of submerged mechanical devices. Each device includes...
A kite system includes a kite and a ground station. The ground station includes a sensor that can be...
Thermodynamic and operating characteristics of high temperature liquid mercury cathode ion thruster
A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silico...
Exemplary deployable sheet material systems may be configured to stow and deploy sheet material. The...
A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel...
An apparatus for generating flight-optimizing trajectories for a first aircraft includes a receiver ...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
An aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser ...
Systems and methods for lightweight, customizable antenna with improved performance and mechanical p...
An electric propulsion machine includes an ion thruster having a discharge chamber housing a large s...
An improved acoustic liner for turbine engines is disclosed. The acoustic liner may include a straig...
An amorphous robot includes a compartmented bladder containing fluid, a valve assembly, and an outer...
An actuator includes a housing assembly, a ball nut, a ball screw, and a ball screw stop. The ball n...
A lower robotic arm includes a base structure, a plurality of digits, and a plurality of tendons. Th...
A power generation system includes a plurality of submerged mechanical devices. Each device includes...
A kite system includes a kite and a ground station. The ground station includes a sensor that can be...
Thermodynamic and operating characteristics of high temperature liquid mercury cathode ion thruster
A simultaneous ohmic contact to silicon carbide includes a mixture of platinum, titanium, and silico...
Exemplary deployable sheet material systems may be configured to stow and deploy sheet material. The...
A combustor is provided. The combustor may comprise an axial fuel delivery system, and a radial fuel...
An apparatus for generating flight-optimizing trajectories for a first aircraft includes a receiver ...
A nozzle assembly for a dual gas turbine engine propulsion system includes a housing mountable proxi...
An aircraft includes a propulsor supported within an aft portion of the fuselage. A thrust reverser ...
Systems and methods for lightweight, customizable antenna with improved performance and mechanical p...