Abstract: An antenna is provided for use with a vehicle that includes a body that is encased by a thermal protection system (TPS). An opening extends through the TPS and the vehicle body, and an antenna assembly and a seal member are positioned within the opening. The seal member extends about the antenna assembly and is radio frequency (RF) opaque. A window extends across the opening to retain the antenna assembly and seal member within the opening. The window is RF transparent.

Abstract: A method of and a system for controlling personal air vehicle (PAV) traffic provides a take-off-and-landing zone, and a forward flight zone. The take-off-and-landing zone may be from the ground up to a first altitude. The forward flight zone may be from the first altitude up to a second altitude. A maximum airspeed is provided in the take-off-and-landing zone. Minimum and maximum airspeeds are provided in the forward flight zone. In the forward flight zone there is a single heading for each altitude. Any change in heading must be accompanied by a change in altitude.

Abstract: A system and method of constructing a system for delivering cargo by airdrop are provided. In short, the system uses rotor blades to slow the descent of cargo dropped from an aircraft. In one example of one embodiment, a frame is secured to a cargo pallet and at least one rotor blade is secured to the frame. The rotor blade is secured to the frame in a position such that it causes the cargo pallet and the frame to rotate in air when dropped from an elevation. In another embodiment, the rotor blade may be extendable and extend during flight.

Abstract: A system and method of constructing a system for delivering cargo by airdrop are provided. In short, the system uses rotor blades to slow the descent of cargo dropped from an aircraft. In one example of one embodiment, a frame is secured to a cargo pallet and at least one rotor blade is secured to the frame. The rotor blade is secured to the frame in a position such that it causes the cargo pallet and the frame to rotate in air when dropped from an elevation. In another embodiment, the rotor blade may be extendable and extend during flight.

Abstract: A method of and a system for controlling personal air vehicle (PAV) traffic provides a take-off-and-landing zone, and a forward flight zone. The take-off-and-landing zone may be from the ground up to a first altitude. The forward flight zone may be from the first altitude up to a second altitude. A maximum airspeed is provided in the take-off-and-landing zone. Minimum and maximum airspeeds are provided in the forward flight zone. In the forward flight zone there is a single heading for each altitude. Any change in heading must be accompanied by a change in altitude.

Abstract: A method of and a system for controlling personal air vehicle (PAV) traffic provides a take-off-and-landing zone, and a forward flight zone. The take-off-and-landing zone may be from the ground up to a first altitude. The forward flight zone may be from the first altitude up to a second altitude. A maximum airspeed is provided in the take-off-and-landing zone. Minimum and maximum airspeeds are provided in the forward flight zone. In the forward flight zone there is a single heading for each altitude. Any change in heading must be accompanied by a change in altitude.

Abstract: A latching system includes a flexible hydraulic latch male portion, and a receiving rail female portion. The receiving rail female portion receives the hydraulic latch male portion therein. The latching system includes a hydraulic system for providing hydraulic fluid into the flexible hydraulic latch. The latching system includes a controlling device for controlling operation and hydraulic fluid insertion by the hydraulic system into the flexible hydraulic latch. The latching system includes an ejection system coupled to the hydraulic system or flexible hydraulic latch for reducing hydraulic fluid pressure within the flexible hydraulic latch during an ejection evolution.

Abstract: A system and method for attaching an injection molded canopy to a vehicle is provided. The system includes a canopy rail attached to the vehicle and an injection-molded canopy that is molded to be securely received by the canopy rail. The canopy is a polycarbonate or acrylic frameless canopy. The system also includes a seal, a canopy position sensor, a sealing component, and a canopy handle for controlling position of the canopy. The sealing component inflates the one or more seals with one of a liquid or gas when the canopy is sensed in the closed position. The system also includes a ground sensor. The sealing component deflates the seal if the canopy handle is in an open position and the aircraft is on the ground.

Abstract: A system and method for attaching an injection molded canopy to a vehicle is provided. The system includes a canopy rail attached to the vehicle and an injection-molded canopy that is molded to be securely received by the canopy rail. The canopy is a polycarbonate or acrylic frameless canopy. The system also includes a seal, a canopy position sensor, a sealing component, and a canopy handle for controlling position of the canopy. The sealing component inflates the one or more seals with one of a liquid or gas when the canopy is sensed in the closed position. The system also includes a ground sensor. The sealing component deflates the seal if the canopy handle is in an open position and the aircraft is on the ground.

Abstract: A latching system includes a flexible hydraulic latch male portion, and a receiving rail female portion. The receiving rail female portion receives the hydraulic latch male portion therein. The latching system includes a hydraulic system for providing hydraulic fluid into the flexible hydraulic latch. The latching system includes a controlling device for controlling operation and hydraulic fluid insertion by the hydraulic system into the flexible hydraulic latch. The latching system includes an ejection system coupled to the hydraulic system or flexible hydraulic latch for reducing hydraulic fluid pressure within the flexible hydraulic latch during an ejection evolution.