Skip to content
Vincony — fast, managed web hosting for your next site
The Pilots Desk
Reconnaissancereconnaissance aircraft by Lockheed

Lockheed A-12

Lockheed A-12

The Lockheed A-12 is a retired high-altitude, Mach 3+ reconnaissance aircraft built for the United States Central Intelligence Agency (CIA) by Lockheed's Skunk Works, based on the designs of Clarence "Kelly" Johnson. The aircraft was designated A-12, the twelfth in a series of internal design efforts for "Archangel", the aircraft's internal code name. In 1959, it was selected over Convair's FISH and Kingfish designs as the winner of Project GUSTO, and was developed and operated under Project Oxcart. The CIA's representatives initially favored Convair's design for its smaller radar cross-section, but the A-12's specifications were slightly better and its projected cost was much lower. The companies' respective track records proved decisive. Convair's work on the B-58 had been plagued with delays and cost overruns, whereas Lockheed had produced the U-2 on time and under budget. In addition, Lockheed had experience running a highly classified "black" project. The A-12 was produced from 1962 to 1964 and flew from 1963 to 1968. It was the precursor to the twin-seat U.S. Air Force YF-12 prototype interceptor, M-21 launcher for the D-21 drone, and the SR-71 Blackbird, a slightly longer variant able to carry a heavier fuel and camera load. The A-12 began flying missions in 1967 and its final mission was in May 1968; the program and aircraft were retired in June. The program was officially revealed in the mid-1990s. A CIA officer later wrote, "Oxcart was selected from a random list of codenames to designate this R&D and all later work on the A-12. The aircraft itself came to be called that as well." The crews named the A-12 the Cygnus, suggested by pilot Jack Weeks to follow the Lockheed practice of naming aircraft after celestial bodies.

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Category
Reconnaissance
First flight
1962-04-26
Length
30.97 m
Wingspan
16.95 m

Specifications

Cruise speed
3.1 kt
Max speed
3.3 kt
Range
2,500 nm
Service ceiling
85,000 ft
Rate of climb
11,800 ft/min
Max takeoff weight
117,000 lb
Fuel capacity
10,590 US gal
Powerplant
Pratt & Whitney JT11D-20B
Engines
2
Seats
1
Length
101.6 ft
Wingspan
55.6 ft
Height
18.5 ft
Number built
13

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.