TSR-2 in the context of "Nuclear weapons delivery"

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⭐ Core Definition: TSR-2

The British Aircraft Corporation TSR-2 was a cancelled supersonic strike and reconnaissance aircraft designed by the British Aircraft Corporation (BAC). It was under development throughout the late 1950s and early 1960s for the Royal Air Force (RAF); the TSR-2 designation came from "Tactical Strike and Reconnaissance, Mach 2".

The TSR-2 arose from the issuing of General Operational Requirement 339 (GOR.339) in November 1956, which sought a successor to the English Electric Canberra that would perform both conventional and tactical nuclear weapons delivery, be able to penetrate well-defended frontline areas at low altitudes and very high speeds, and attack high-value targets in rear areas. Another intended combat role was to provide high-altitude, high-speed stand-off, side-looking radar and photographic imagery and signals intelligence, aerial reconnaissance. On 1 January 1959, the project received its official go-ahead; early work was undertaken by Vickers-Armstrong in cooperation with English Electric, before Britain's aircraft industry underwent consolidation to create BAC. However, as some contributing manufacturers were employed directly by the Ministry rather than through BAC, this led to communication difficulties and cost overruns. On 27 September 1964, test pilot Roland Beamont performed the type's maiden flight.

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TSR-2 in the context of Terrain-following radar

Terrain-following radar (TFR) is a military aerospace technology that allows a very-low-flying aircraft to automatically maintain a relatively constant altitude above ground level and therefore make detection by enemy radar more difficult. It is sometimes referred to as ground hugging or terrain hugging flight. The term nap-of-the-earth flight may also apply but is more commonly used in relation to low-flying military helicopters, which typically do not use terrain-following radar.

TFR systems work by scanning a radar beam vertically in front of the aircraft and comparing the range and angle of the radar reflections to a pre-computed ideal manoeuvring curve. By comparing the distance between the terrain and the ideal curve, the system calculates a manoeuvre that will make the aircraft clear the terrain by a pre-selected distance, often on the order of 100 metres (330 ft). Using TFR allows an aircraft to automatically follow terrain at very low levels and high speeds.

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