Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)Type: Turbojet Thrust: 13,100 N (2,950 lb) at 16,500 rpm Compressor: 8-stage axial Combustor: Annular Turbine: 2-stage axial Weight: 178 kg (392 lb)This object is not on display at the National Air and Space Museum.
Apollo 11 was a global event. What did that historic mission mean to you? GE's Customer Web Center allows you to browse engine shop manuals, illustrated parts catalogs, service bulletins and more with just a click. Specializing in Honeywell TFE731, General Electric CJ610 / CF700 / J85 and Pratt & Whitney Canada JT15D overhaul, repair, inspection and test cell testing.
Our scientists are involved in current research focused on the Martian climate and geology. It is either on loan or in storage.The CJ610, derived from General Electric's J85 military turbojet engine, powered the majority of the first generation of business jet aircraft during the 1960s and early 1970s.
Military versions produce up to 2,950 lb f (13.1 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 300 to 500 pounds (140 to 230 kg). The first model in the series, the CJ610-1, was certificated in late-1961 at 12,700 N (2,850 lb) thrust, and powered the Aero Commander Jet Commander 1121, which first flew in January 1963.Other CJ610 models powered the Learjet Models 23/24/25/28/29, Hamburger Flugzeugbau HFB 320 (Hansa), and Israel Aircraft Industries Model 1123 Westwind. The General Electric J85 is a small single-shaft turbojet engine. Thank you. × 2 ft. 6 1/2 in.)
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