초록 ▼

An unmanned air vehicle system which is intended for launch from a platform such as an aircraft or a ship and to follow other than a ballistic trajectory includes a pair of substantially similar air vehicles in a tandem relationship. A unitary tubular airframe is provided coextensive with both air v

An unmanned air vehicle system which is intended for launch from a platform such as an aircraft or a ship and to follow other than a ballistic trajectory includes a pair of substantially similar air vehicles in a tandem relationship. A unitary tubular airframe is provided coextensive with both air vehicles. The nose of a second air vehicle is nested in the tail member of a first air vehicle. A rocket booster is mounted in the tail of the second air vehicle and ignited for launch of both air vehicles as a unit. Thereafter, a pyrotechnic separating mechanism is actuated for bisecting the tubular airframe intermediate the tail member of the first air vehicle and the nose of the second air vehicle. Following separation, each air vehicle has a gas turbine engine which is ignited for powering its associated air vehicle to its destination. Electrical connections from the launch platform to the vehicle system are made to the first air vehicle and the second air vehicle is, in turn, electrically connected to the first.

대표청구항 ▼

An unmanned air vehicle system intended to be launched from an air-to-air missile launch station on an aircraft and to follow other than a ballistic trajectory comprising: first and second substantially similar air vehicles, each including a central body section having a longitudinal axis, and being

An unmanned air vehicle system intended to be launched from an air-to-air missile launch station on an aircraft and to follow other than a ballistic trajectory comprising: first and second substantially similar air vehicles, each including a central body section having a longitudinal axis, and being of substantially constant diameter extending from a streamlined nose section at a forward end thereof to a tail section at an aft end thereof, said tail section having a nesting cavity therein for receiving, in nesting relationship, said nose section of said second air vehicle such that said first and second air vehicles are positioned in a tandem relationship with their longitudinal axes aligned; each of said vehicles including airfoils mounted on and extending outwardly from the respective main body section for providing both lift and control; booster rocket means mounted on said aft end of said second air vehicle for initiating free flight of said first and second air vehicles as a unit; separation means selectively operable for separating said first and second air vehicles after free flight has been initiated; and first and second main propulsion means for independently propelling said first and second air vehicles, respectively, after operation of said separation means.