Patent classifications
B64D17/22
EJECTION PROTECTION BLACK BOX SYSTEM AND METHOD
The ejection protection black box is a device that is wired to the computers and engines of an aircraft. The ejection protection black box is able to detect any malfunction that may cause an airplane to crash. In the event of a malfunction, the black box will automatically eject from a chute located on the aircraft safely before impact. The ejection protection black box is further equipped to detect missiles or bombs that may be headed towards an aircraft.
WATER LANDING PARACHUTE TRAP AND METHOD
Systems and methods for aerially delivering cargo into a body of water while avoiding parachute entrapment and entanglement are described. The system includes a parachute having a canopy and suspension lines. The system further includes a weight coupled to a first end of the suspension lines and a ring that is configured to float in the body of water. The weight is coupled to the cargo, and the ring is disposed between the weight and the canopy with the suspension lines passing through the center of the ring.
WATER LANDING PARACHUTE TRAP AND METHOD
Systems and methods for aerially delivering cargo into a body of water while avoiding parachute entrapment and entanglement are described. The system includes a parachute having a canopy and suspension lines. The system further includes a weight coupled to a first end of the suspension lines and a ring that is configured to float in the body of water. The weight is coupled to the cargo, and the ring is disposed between the weight and the canopy with the suspension lines passing through the center of the ring.
Near-space operation systems
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
Near-space operation systems
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
NEAR-SPACE OPERATION SYSTEMS
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
NEAR-SPACE OPERATION SYSTEMS
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
Near-space operation systems
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
Near-space operation systems
A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.
IMU POD AND METHOD OF RETRIEVAL OF THE SAME
A pod assembly which includes a pod and an inertial measurement unit positioned within the pod. The pod assembly further includes deceleration hardware associated with the pod. A method for using a pod assembly, includes a step of securing the pod assembly, which includes a pod and an inertial measurement unit contained within the pod, to an aircraft and a step of operating the aircraft with the inertial measurement unit operating sensing movement and alignment of the pod and storing data corresponding to the sensed movement and alignment of the pod on a data collection assembly connected to the inertial measurement unit. The method further includes a step of releasing the pod assembly from the aircraft and a step of utilizing deceleration hardware associated with the pod to reduce rate of descent of the pod assembly released from the aircraft.