
General Electric J85 - Wikipedia
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 …
Long Live the J85, GE’s “Little Tough Guy” - GE Aerospace
2020年6月1日 · No engine in jet propulsion is quite like GE’s tiny J85 turbojet. Originally designed in 1954, the J85 is expected to power U.S. military aircraft until at least 2040. That’s not a …
GE航空的“小硬汉”发动机:今年65周岁,还将服役20年 - 知乎
J85直径约18英寸(46厘米),长45英寸(110厘米),自重396-421磅(180-191千克),推重比达8:1,多年来J85的推重比在航空发动机中都是最高的。 因此,在GE航空内部被称为“小硬 …
General Electric J85 Turbojet Engine - Fight's On
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 …
General Electric J85 - Wikiwand
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 lbf (22 kN). The …
Turbojet Engine, Cutaway, General Electric J85-GE-17A
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 …
J85 - StandardAero
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 …
J85 - GlobalSecurity.org
It is powered by two General Electric J85 afterburning turbojet engines located close together in the aft fuselage, each with 3850 lb of thrust. The first T-38 built flew in 1959. More than...
General Electric J85 - Wikiwand
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 lbf (22 kN). The …
J85-21 - AeroTurbine
The J85-GE-21 is a lightweight, single-spool turbojet engine with a rated non-afterburning thrust of 3500 lbf (15.5 kilonewtons). General Characteristics. Type: Afterburning turbojet engine; …
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