Add to ORKGThis invention is a tubular shaped guideway for high-speed air-cushioned supported vehicles. The tubular guideway is split and separated such that the sides of the guideway are open. The upper portion of the tubular guideway is supported above the lower portion by truss-like structural members. The lower portion of the tubular guideway may be supported by the terrain over which the vehicle travels, on pedestals or some similar structure
A low mass rolling element with a lightweight core and hollow center was developed for use in bearin...
Equipotential space suits utilizing mechanical aids to minimize astronaut energy at bending joint
Black body radiometer design with temperature sensing and cavity heat source cone windin
Hermetic sealing device for ends of tubular bodies during materials testing operation
Mating flat surfaces inhibit leakage of a fluid around a stationary shaft. A spiral groove pattern p...
Mating flat surfaces inhibit leakage of a fluid around a stationary shaft. A spiral groove produces ...
A waste collection system for use in a reduced gravity including a seat having an opening centrally ...
System for removing and repairing spacecraft control thrusters by use of portable air lock
An air speed and attitude probe characterized by a pivot shaft normally projected from a data boom a...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
High impact pressure regulator having minimum number of lightweight movable element
In addition to fixed and variable bleed devices provided for controlling the position of a terminal ...
Liquid-vapor interface seal design for turbine rotating shafts including helical and molecular pumps...
A supporting frame for a load, such as one or more telescopes, is isolated from all multi-gravitatio...
A parachute fabric for aerodynamic decelerator applications is described. The fabric will permit dep...
A low mass rolling element with a lightweight core and hollow center was developed for use in bearin...
Equipotential space suits utilizing mechanical aids to minimize astronaut energy at bending joint
Black body radiometer design with temperature sensing and cavity heat source cone windin
Hermetic sealing device for ends of tubular bodies during materials testing operation
Mating flat surfaces inhibit leakage of a fluid around a stationary shaft. A spiral groove pattern p...
Mating flat surfaces inhibit leakage of a fluid around a stationary shaft. A spiral groove produces ...
A waste collection system for use in a reduced gravity including a seat having an opening centrally ...
System for removing and repairing spacecraft control thrusters by use of portable air lock
An air speed and attitude probe characterized by a pivot shaft normally projected from a data boom a...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
High impact pressure regulator having minimum number of lightweight movable element
In addition to fixed and variable bleed devices provided for controlling the position of a terminal ...
Liquid-vapor interface seal design for turbine rotating shafts including helical and molecular pumps...
A supporting frame for a load, such as one or more telescopes, is isolated from all multi-gravitatio...
A parachute fabric for aerodynamic decelerator applications is described. The fabric will permit dep...
A low mass rolling element with a lightweight core and hollow center was developed for use in bearin...
Equipotential space suits utilizing mechanical aids to minimize astronaut energy at bending joint
Black body radiometer design with temperature sensing and cavity heat source cone windin