The Martin RB-57D Canberra was a specialized high-altitude strategic reconnaissance aircraft that the Glenn L. Martin Company developed from its B-57 Canberra tactical bomber, itself a license-built version of the English Electric Canberra. It grew out of a December 1952 United States Air Force study for a jet reconnaissance aircraft able to work at about 65,000 feet, and it first flew on 5 November 1955. Martin gave it a much larger wing, new J57 turbojet engines, wet-wing fuel cells and a lightened, unarmed airframe, and only twenty were built, in four variants. The type flew reconnaissance and air sampling missions for the Air Force and for Taiwanese crews under CIA sponsorship, and one was shot down in 1959 in the first successful shoot-down of an aircraft by a surface-to-air missile. Wing fatigue ended front-line use, but converted EB-57D aircraft served as radar targets until the last was retired in 1979.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EnginePratt & Whitney J57-P-9 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Derived From
Source Martin RB-57D Canberra (Wikipedia)
Exemplifies
Source Martin RB-57D Canberra (Wikipedia)
Of Make
Source Martin RB-57D Canberra (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Martin RB-57D Canberra (Wikipedia)Retirement, wing designQuote, Retirement, wing design
Martin had designed the wings for only 500 flight hours and many of them had already exceeded that limit
Originated In
Also in Geography Atlas: where this subject originated.
Source Martin RB-57D Canberra (Wikipedia)Development, requirement, country of originQuote, Development, requirement, country of origin
It originated in a December 1952 USAF study funded by the Wright Air Development Center
Sources
1. Martin RB-57D Canberra (Wikipedia)
Production, first flight
The first RB-57D flew on 5 November 1955.
Lead
is a specialized high-altitude strategic reconnaissance aircraft developed from the Martin B-57 Canberra tactical bomber
Development, requirement
for a turbojet-powered special reconnaissance aircraft
Retirement
until the last was retired in July 1979 due to wing-spar fractures
Production
Only 20 RB-57Ds were built
Specifications, performance
Maximum speed: 520 kn (600 mph, 966 km/h) at 45,000 ft (14,000 m)
Specifications, general characteristics
Max takeoff weight: 59,000 lb (26,760 kg) approximately
Specifications, powerplant
Pratt & Whitney J57-P-9 turbojets, 10,000 lbf (44 kN) thrust each
Retirement, wing design
Martin had designed the wings for only 500 flight hours and many of them had already exceeded that limit
Development, requirement, country of origin
It originated in a December 1952 USAF study funded by the Wright Air Development Center
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