J85 General Electric Turbojet Engine

The gen eral elec tric j85 is a small sin gle shaft tur bo jet en gine.

J85 general electric turbojet engine.

The en gine de pend ing upon ad di tional equip ment and spe cific model weighs from 300 to 500 pounds 140 to 230 kg. Military versions produce up to 2 950 lbf13 kn of thrust dry afterburning variants can reach up to 5 000 lbf 22 kn. 26 upi aero turbine has received a 128 7 million contract to provide j85 ge 5 21 engine component overhauls for the u s. Mil i tary ver sions pro duce up to 2 950 lb f 13 1 kn of thrust dry af ter burn ing vari ants can reach up to 5 000 lb f 22 kn.

The general electric j85is a small single shaft turbojet engine. The engine depending upon additional equipment and specific model weighs from 300. The engine depending upon additional equipment and specific model weighs from 300 to 500 pounds 140 to 230 kg. Afterburning variants can reach up to 5 000 lbf 22 kn.

The design team wrapped a small highly aerodynamic fighter around two compact and high thrust general electric j85 engines focusing on performance and a low cost of maintenance. On november 28 1954 general electric was awarded a usaf development. Military versions produce up to 2 950 lbf 13 1 kn of thrust dry. The general electric j85 is a small single shaft turbojet engine.

In late 1953 general electric began a design study of a high thrust to weight ratio turbojet engine. Military versions produce up to 2 950 lb f 13 1 kn of thrust dry. The general electric cj610 is a non afterburning turbojet engine derived from the military j85 and is used on a number of civilian business jets. General electric j85 turbojet engine the j85 was originally designed to power a large decoy missile the mcdonnell adm 20 quail.

The general electric j85 is a small single shaft turbojet engine. Afterburning variants can reach up to 5 000 lb f 22 kn.