The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN ) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from …

Specific examples of technology insertion are detailed, including a discussion of the innovative program leading to upgrade of the J85-powered T-38 fleet and options for the rest of the world's air forces.

Jun 1, 2020 · For many years, the J85 had the highest thrust-to-weight ratio (8:1) of any jet engine in aviation. Let’s just call it “The Little Tough Guy.”

The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 2,950 lbf (13.1 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). The engine, depending upon additional equipment and specific model, weighs from …

The J85 was the first U.S. small turbine engine to go into production with an afterburner. The most important applications were the Northrop T-38 Talon, the first supersonic trainer, and Northrop F-5 Freedom Fighter, a low-cost fighter used by many nations from the 1960s through the 1980s.

J85 Engine Expertise. The J85-GE engine, known as the “Little Tough Guy,” powers the F-5 fighter jet and T-38 trainer, with StandardAero providing life cycle-optimized maintenance solutions to extend their operational life.

The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3500lk=onNaNlk=on of thrust dry; afterburning variants can reach up to 5000lb-f. The engine, depending upon additional equipment and specific model, weighs from 300lb500lb.

introduced in 1960, to power "an efficient supersonic light fighter", the j85 turbojet is a powerplant providing between 2,850 and 5,000 lb. of thrust to a-37 dragonfly, cf-5 freedom fighter, cf-116 freedom fighter, ct-114 tutor, f-5 tiger aircraft.

Apr 6, 2025 · Details on the GE J85-GE-5A aircraft engine, based on current FAA records. Data presented on this website is sourced directly from official Federal Aviation Administration (FAA) records.

The J85-GE-21C, manufactured by the US General Electric Company, Is a turbojet engine with a 9-stage axial-flow compressor at 8:1 pressure ratio. Equipped with annular combustion chambers followed by one 2-stage coaxial constant-speed turbine, the engine was installed on the F …