|
The Jordan Falcon, a joint venture between the King Abdulla Design and Development Bureau and Jordan Aerospace Industries, is a compact tactical unmanned aerial vehicle (UAV) capable of performing a wide range of aerial robotic applications. It performs real-time day and night reconnaissance, remote sensing, surveillance and target acquisition up to a range of 50 km. The Jordan Falcon is powered by a quiet 200cc 2-stroke engine burning a conventional gas/oil mixture with fuel for a 4-hour flight stored in the aircraft's fuselage tank. Additional fuel tanks may be equipped to provide added capacity. A generator and an emergency onboard batteries power the aircraft and payload. Its heading, altitude, airspeed and GPS waypoint navigation are fully controlled by an autopilot. A 5-watt video/telemetry microwave datalink transmits real-time imagery and vehicle telemetry back from the UAV at ranges up to 50 km. ==Specifications== * Stall Speed, SLS - 80 km/h (50 mph) * Maximum Speed, SLS - 180 km/h (110 mph) * Cruise Speed, SLS - 120 km/h (75 mph) * Operational Maximum Range (still air) - 450 km/h * Operational Endurance - 4 h * MGTOW - 60 kg (132 lb) * Empty Weight - 40 kg (88 lb) * Maximum Fuel - 14 kg (30 lb) * Payload - 6 kg (13 lb) 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Jordan Falcon」の詳細全文を読む スポンサード リンク
|