The SR-71 remained the world's fastest and highest-flying operational manned aircraft throughout its career. From an altitude of 80,000 ft (24 km) it could survey 100,000 square miles per hour (72 square kilometers per second) of the Earth's surface. On 28 July 1976, an SR-71 broke the world record for its class: an absolute speed record of 2,193.1669 mph (3,529.56 km/h), and a US "absolute altitude record" of 85,068.997 feet (25,929 m). Several planes exceeded this altitude in zoom climbs but not in sustained flight. When the SR-71 was retired in 1990, one was flown from its birthplace at United States Air Force Plant 42 in Palmdale, California to go on exhibit at what is now the Smithsonian Institution's Steven F. Udvar-Hazy Center (an annex of the National Air & Space Museum) in Chantilly, Virginia. The Blackbird, piloted by Colonel Ed Yielding and Lt. Col. J.T. Vida, set a coast-to-coast speed record at an average 2,124 mph (3,418 km/h). The entire trip was reported as 68 minutes and 17 seconds. Three additional records were set within segments of the flight, including a new absolute top speed of 2,242 mph measured between the radar gates set up in St. Louis and Cincinnati. These were accepted by the National Aeronautic Association (NAA), the recognized body for aviation records in the United States. An enthusiast site devoted to the Blackbird lists a record time of 64 minutes. The SR-71 also holds the record for flying from New York to London: 1 hour 54 minutes and 56.4 seconds, set on 1 September 1974. This is only Mach 2.68, well below the declassified figure of 3.0+. (For comparison, commercial Concorde flights took around 3 hours 20 minutes, and the Boeing 747 averages 6 hours.)
General characteristics
Crew: 2
Payload: 3,500 lb (1,600 kg) of sensors
Length: 107 ft 5 in (32.74 m)
Wingspan: 55 ft 7 in (16.94 m)
Height: 18 ft 6 in (5.64 m)
Wing area: 1,800 ft2 (170 m2)
Empty weight: 67,500 lb (30 600 kg)
Loaded weight: 170,000 lb (77 000 kg)
Max takeoff weight: 172,000 lb (78 000 kg)
Powerplant: 2× Pratt & Whitney J58-1 continuous-bleed afterburning turbojets, 32,500 lbf (145 kN) each
Wheel track: 16 ft 8 in (5.08 m)
Wheel base: 37 ft 10 in (11.53 m)
Aspect ratio: 1.7
Performance
Maximum speed: Mach 3.3+ (2,200+ mph, 3530+ km/h) at 80,000 ft (24,000m)
Range:
Combat: 2,900 nm (5400 km)
Ferry: 3,200 nm (5,925 km)
Service ceiling: 85,000 ft (25,900m, 16 miles)
Rate of climb: 11,810 ft/min (60 m/s)
Wing loading: 94 lb/ft2 (460 kg/m2)
Thrust/weight: 0.382
Crew: 2
Payload: 3,500 lb (1,600 kg) of sensors
Length: 107 ft 5 in (32.74 m)
Wingspan: 55 ft 7 in (16.94 m)
Height: 18 ft 6 in (5.64 m)
Wing area: 1,800 ft2 (170 m2)
Empty weight: 67,500 lb (30 600 kg)
Loaded weight: 170,000 lb (77 000 kg)
Max takeoff weight: 172,000 lb (78 000 kg)
Powerplant: 2× Pratt & Whitney J58-1 continuous-bleed afterburning turbojets, 32,500 lbf (145 kN) each
Wheel track: 16 ft 8 in (5.08 m)
Wheel base: 37 ft 10 in (11.53 m)
Aspect ratio: 1.7
Performance
Maximum speed: Mach 3.3+ (2,200+ mph, 3530+ km/h) at 80,000 ft (24,000m)
Range:
Combat: 2,900 nm (5400 km)
Ferry: 3,200 nm (5,925 km)
Service ceiling: 85,000 ft (25,900m, 16 miles)
Rate of climb: 11,810 ft/min (60 m/s)
Wing loading: 94 lb/ft2 (460 kg/m2)
Thrust/weight: 0.382
more info here: http://en.wikipedia.org/wiki/SR-71_Blackbird
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