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| Name | SR-71 Blackbird |
| Manufacturer | Lockheed Skunk Works |
| Country of Origin | United States |
| Introduction / In Service Since | 1966 |
| Status | Retired |
| Category | Strategic reconnaissance aircraft |
| Crew | 2 |
| Unit Cost | No current procurement price; historical program cost varied |
| Length | 107.4 ft |
| Wingspan | 55.6 ft |
| Height | 18.5 ft |
| Wing Area | Approximately 1,800 sq ft |
| Empty Weight | Approximately 60,000 lb |
| Maximum Takeoff Weight (MTOW) | Approximately 140,000 lb |
| Maximum Speed | Mach 3.2+ |
| Range | 2,000 miles unrefueled |
| Combat Radius | Not applicable to reconnaissance mission |
| Service Ceiling | More than 85,000 ft |
| Rate of Climb | Not consistently published |
| Engine Type | 2 × Pratt & Whitney J58 |
| Thrust (per engine) | 32,500 lb with afterburner |
| Total Thrust | 65,000 lb with afterburner |
| Internal Payload Capacity | Mission-specific reconnaissance equipment |
| Weapons Bay | Sensor bays |
| Compatible Weapons | None |
| Hardpoints | None |
| Radar System | No conventional search radar |
| Navigation | Advanced inertial navigation and mission navigation systems |
| Electronic Warfare (EW) | Electronic intelligence and electronic countermeasures |
| Stealth Features | Reduced radar cross-section design, specialized shaping and coatings |
| Primary Operator | U.S. Air Force |
| Conflict Usage | Vietnam War and Cold War reconnaissance |
| Notable Missions | Strategic intelligence and photographic reconnaissance |
| Variants | SR-71A, SR-71B, SR-71C |
| Successor / Future Replacement | No direct operational replacement |
| Notable Features | Titanium construction, Mach 3+ cruise, high-altitude reconnaissance |
| Estimated Operational Life | 1966 to 1990 in primary USAF service; NASA operations continued into 1999 |
The SR-71 Blackbird was a U.S. long-range strategic reconnaissance aircraft designed to collect intelligence at extreme speed and altitude. Developed by Lockheed’s Advanced Development Company, known as the Skunk Works, under Clarence Kelly Johnson, the aircraft evolved from the A-12 and YF-12 programs. The SR-71 first flew on December 22, 1964, and entered U.S. Air Force service in 1966.
Built primarily from titanium alloys, the Blackbird was engineered to withstand the intense aerodynamic heating generated during sustained Mach 3 flight. Its mission equipment included photographic cameras, electronic intelligence systems, and defensive electronic countermeasures. It carried no conventional weapons and relied on speed, altitude, reduced radar observability, and electronic countermeasures for survivability.
Lockheed Skunk Works, now part of Lockheed Martin, developed and manufactured the SR-71 for the U.S. Air Force. The aircraft operated primarily from Beale Air Force Base, Kadena Air Base in Okinawa, and RAF Mildenhall.
The SR-71 could cruise at more than Mach 3, with NASA documenting a maximum speed above Mach 3.2. Its July 1976 record reached 2,193.167 mph, while its service ceiling exceeded 85,000 feet. Published figures vary by source and mission configuration, with NASA listing approximately 2,000 miles unrefueled and the U.S. Air Force National Museum listing more than 2,900 statute miles.
The SR-71 has no current procurement price because production and operational service ended decades ago. Operating costs were substantial, reflecting specialized JP-7 fuel, aerial refueling, maintenance, and complex support requirements. One Air Force account cites approximately $85,000 per flight hour during its later operational era.
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