Αποτελέσματα Αναζήτησης
Prototype single-engined, strategic reconnaissance aircraft for CIA and USAF. Designated as Article 341. by the CIA with a non-standard serial number. As U-2, production version with engine upgrade. Several used for CIA ops with civil regs. As U-2A, engine upgrade. Several used for CIA ops with civil regs.
TR-1A – A third production batch of U-2R aircraft built for high-altitude tactical reconnaissance missions with side-looking radar, new avionics, and improved ECM equipment; 33 built. Re-designated U-2S after the fall of the Soviet Union.
A tactical reconnaissance version, the TR-1A, first flew in August 1981 and was delivered to the Air Force the next month. Designed for stand-off tactical reconnaissance in Europe, the TR-1 was structurally identical to the U-2R.
17th Reconnaissance Wing aircraft, landing at its Alconbury base. Operated by 95 RS from RAF Alconbury. Later redesignated U-2S. This TR-1A was operated by 95th RS from RAF Alconbury. There, it crashed on 24 April 1990. Fortunately, it was rebuilt as a TU-2S and became operational again as of 1994.
Real-time aircraft tracking on 1090 MHz band; Patented FPGA-In-The_Loop TM technology with the capability of receiving thousands of frames per second; Integrated high quality GNSS position source and barometric altitude sensor; 0.25, 0.5 or 1 Watt RF output power; Implemented MAVLink and AERO protocol; Low-power consumption and low weight design
TR-1A may refer to A "tactical recon" variant of the US Lockheed U-2 spy plane; A variant of the Lyul'ka TR-1 1940's Soviet turbojet engine
Lockheed met this demand by taking the original idea of the U-2 and building an entirely new and much bigger aircraft, the TR-1. The new plane was 12 feet, 9 inches longer, had a span 23 feet greater, and could fly 10,000 feet higher than its predecessor.
