SR-71

The SR-71 is a delta-wing aircraft designed and built by Lockheed. They are powered by two Pratt and Whitney J-58 axial-flow turbojets with afterburners, each producing 32,500 pounds of thrust. Studies have shown that less than 20 percent of the total thrust used to fly at Mach 3 is produced by the basic engine itself. The balance of the total thrust is produced by the unique design of the engine inlet and "moveable spike" system at the front of the engine nacelles, and by the ejector nozzles at the exhaust which burn air compressed in the engine bypass system.

The Blackbird weighs about 34 tons empty, and can carry another 20 tons of special JP-7 jet fuel (enough for about two hours of flight time) in its fuselage and wing tanks. In flight, the fuel is redistributed automatically to maintain the plane's center of gravity and load specifications. Because the Blackbird was designed to expand during flight, it has had a history of fuel tank leaks on the ground.
https://fas.org/irp/program/collect/sr-71.htm