초록 ▼

An air-based vertical launch system is described by means of which ballistic missile defense can be achieved effectively from a large aircraft. A method for ensuring safe missile egress is proposed. A method for ensuring that the missile strikes the ballistic missile payload section is also proposed

An air-based vertical launch system is described by means of which ballistic missile defense can be achieved effectively from a large aircraft. A method for ensuring safe missile egress is proposed. A method for ensuring that the missile strikes the ballistic missile payload section is also proposed. Together, the air basing method employing vertical (or near-vertical) launch and semi-active laser guidance yield an affordable and operationally effective missile defense against both tactical and long-range ballistic missiles. The affordability of missile defense is enhanced by the ability of an aircraft equipped with a vertical launcher to simultaneously carry out several defensive and offensive missions and to provide other capabilities such as satellite launch at other times. Methods for employing an aircraft equipped with a vertical (or near-vertical launcher) and one or more of the proposed egress assurance mechanisms in offensive ground attack missions, mine laying, and satellite launch missions are also proposed.

대표청구항 ▼

What is claimed is: 1. A method for launching UAVs from great standoff comprising the steps of: placing the UAV in a missile bus consisting of a dual-thrust booster with TVC, a GPS-aided INS, a retarding device, a separating shroud, and a UAV initialization device, mounting the missile bus in an ap

What is claimed is: 1. A method for launching UAVs from great standoff comprising the steps of: placing the UAV in a missile bus consisting of a dual-thrust booster with TVC, a GPS-aided INS, a retarding device, a separating shroud, and a UAV initialization device, mounting the missile bus in an approximately vertical position in an aircraft, launching the missile bus to release the UAV at a prescribed location based on GPS coordinates. 2. The method of claim 1 wherein the missile bus is vertically mounted. 3. The method of claim 1 wherein the missile bus is mounted in a tilted position.