发明名称 AIR-LAUNCHABLE AIRCRAFT AND METHOD OF USE
摘要 <p>An air-launched aircraft includes deployable wings, elevons, and vertical fins that deploy from a fuselage during flight. The aircraft may include a control system for operating the elevons, a communication system, and batteries for powering the systems. In addition, the aircraft may include a payload module that mates with an interface in the fuselage. The payload module may include any of a variety of payloads, including cameras, sensors, and/or radar emitters. The aircraft may be powered or unpowered, and may be very small, for example, less than on the order of 10 kg (22 pounds). The aircraft may be employed at a low cost for any of a wide variety of functions, such as surveillance, or as a decoy. The deployable surfaces of the aircraft may be configured to deploy in a pre-determined order, allowing the aircraft automatically to enter controlled flight after being launched in a tumbling mode.</p>
申请公布号 CA2581212(A1) 申请公布日期 2006.04.06
申请号 CA20052581212 申请日期 2005.02.14
申请人 RAYTHEON COMPANY 发明人 KOESSLER, JEFFREY H.;WEBB, GEORGE R.;CORDER, DAVID A.
分类号 B64C39/02;B64C3/56 主分类号 B64C39/02
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