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Turbojet aircraft engine
The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lbf (16 kN) of thrust dry; afterburning variants
General_Electric_J85
Turbojet engine
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. The
General_Electric_CJ610
Turbofan aircraft engine
Thrust-to-weight ratio: 6.6 Related development General Electric CJ610 General Electric J85 Comparable engines General Electric CJ805-23 Related lists List of aircraft
General_Electric_CF700
Topics referred to by the same term
J85 may refer to: General Electric J85, a small single-shaft turbojet engine HMS Seagull (J85), a Halcyon class minesweeper of Royal Navy J85, the Johnson
J85
Trijet supersonic demonstrator aircraft
the Boom Overture supersonic transport airliner. Powered by three General Electric J85 engines, it was initially designed to maintain a speed of Mach 2
Boom_XB-1
Civil series of the J79 turbojet aircraft engine
aft-fan design, the General Electric CF700 used in the Dassault Falcon 20 business jet, which was developed from the General Electric J85 in the same way
General_Electric_CJ805
Experimental vertical take-off and landing (VTOL) jet aircraft
occurred on 24 May 1958. In 1959, its Viper engines were replaced with General Electric J85 engines. That year the aircraft was delivered to the NASA Ames Research
Bell_X-14
Military advanced trainer aircraft by Northrop
General Electric J85-5A turbojet engines were accommodated within the fuselage to exert less drag and produce fewer aerodynamic disturbances. The J85-5A
Northrop_T-38_Talon
Military training aircraft
for the type, as a number of 105 aircraft have been powered by the General Electric J85 engine instead. Swedish Air Force aircraft were remanufactured during
Saab_105
American aircraft engine manufacturer
General Electric Company (d.b.a GE Aerospace) is an American aircraft engine supplier that is headquartered in Evendale, Ohio, outside Cincinnati. It is
GE_Aerospace
American light attack aircraft developed from the T-37 Tweet basic trainer
engine power by replacing its twin Continental J-69 engines with General Electric J85-J2/5 turbojet engines, each capable of generating up to 2,400 lbf
Cessna_A-37_Dragonfly
Iranian advanced turbojet engine
turbojet engine that is reportedly a reverse-engineered copy of the General Electric J85. Revealed in 2016, the engine powers several military aircraft, including
IAIO_Owj
Canadian aircraft engine manufacturer
production contract for the General Electric J85, for use in the Canadair CL-41 Tutor trainer. The first engine, known as the J85-CAN-40, was delivered in
Orenda_Engines
Experimental stealth aircraft
fighter. The aircraft's powerplants were two 2,950-pound (13.1 kN) General Electric J85-GE-4As from the T-2C Buckeye. Because stealth took precedence above
Lockheed_Have_Blue
Jet powered Training aircraft
(13,000 N). The next major revision, the T-2C, was powered by two General Electric J85-GE-4 turbojets, producing 2,950 lbf (13,100 N). The T-2D and T-2E
North_American_T-2_Buckeye
Iranian fighter aircraft
Islamic Republic of Iran Air Force General characteristics Powerplant: 2 × Upgraded Iranian-built General Electric J85 afterburning turbojet engines (with
HESA_Saeqeh
Italian ground-attack aircraft
turbojet engine of this aircraft was replaced by a pair of afterburning General Electric J85 turbojet engines; in contrast to the single-engined predecessor,
Fiat_G.91Y
American homebuilt sport aircraft
thrust as the Hanchettes hoped for, and eventually, they selected the General Electric J85. With this engine producing around four times the thrust of the previous
Viper_Aircraft_ViperJet
Turbofan aircraft engine
The General Electric TF39 was a high-bypass turbofan engine that was developed to power the Lockheed C-5 Galaxy. It was the first high-bypass jet engine
General_Electric_TF39
US lightweight low-cost fighter aircraft
team wrapped a small, highly aerodynamic fighter around two compact General Electric J85 engines, focusing on performance and a low cost of maintenance. Smaller
Northrop_F-5
American startup supersonic aircraft company
demonstrator, designed to fly up to Mach 1.3, and powered by three General Electric J85-15 engines with a total of 12,900 pounds-force [lbf] (57 kN) of thrust
Boom_Technology
Military transport aircraft series by Chase Aircraft, later Fairchild Aircraft
contract the USAF expanded it to allow the mounting of two pod-mounted General Electric J85 turbojets. In 1979, the Royal Thai government, seeking to extend
Fairchild_C-123_Provider
Car propelled by a jet engine
the Pratt & Whitney J60 or the General Electric J85 jet engine.[citation needed] Aero-engined car Drag racing Electric dragster Jet engine JetTrain Jet
Jet_car
American aerial gunship
The AC-119K could be visually distinguished by the addition of two General Electric J85 turbojet engines in underwing pods. The conversions were completed
Fairchild_AC-119
Canceled American military plane project of the 1940s-1950s
401 sq ft (37.2 m2) Gross weight: 38,000 lb (17,237 kg) Powerplant: 6 × General Electric J85 turbojet Performance Maximum speed: Mach 2.3 Project Hummingbird
Republic_AP-100
Proposed American fighter (cancelled 1961)
800 lb (6,260 kg) Gross weight: 23,917 lb (10,849 kg) Powerplant: 8 × General Electric J85-GE-5 turbojets, 2,600 lbf (12 kN) thrust each Performance Maximum
Bell_D-188A
American military transport aircraft
addition of two General Electric M61 Vulcan 20 mm (0.79 in) cannon, improved avionics, and two underwing-mounted General Electric J85-GE-17 turbojet engines
Fairchild_C-119_Flying_Boxcar
Type of aircraft
lightweight fighters, basing its further studies on the use of two small General Electric J85 engines, which allowed a much lighter and cheaper aircraft, with
Northrop_N-102_Fang
SpaceShipOne mother ship
Knight carrier airplane was designed around the twin afterburning General Electric J85 engines, which were selected for their availability and low cost
Scaled Composites White Knight
Scaled_Composites_White_Knight
American experimental VTOL aircraft
XV-5 was powered by two 2,658 lbf (11.8 kN) thrust General Electric J85-GE-5 turbojets. General Electric X353-5 Lift-fans in the wings and a smaller fan
Ryan_XV-5_Vertifan
Iranian training aircraft
construction, with a mid-mounted straight wing). It is powered by a single General Electric J85 jet engine, procured from existing Islamic Republic of Iran Air Force
Owj_Tazarve
1950s British turbojet aircraft engine
Armstrong Siddeley Adder Armstrong Siddeley Sapphire Comparable engines General Electric J85 Ishikawajima-Harima J3 Motorlet M-701 Turbomeca Gabizo Related lists
Armstrong_Siddeley_Viper
Cruise missile
to weight ratio goal of 10:1. General Electric was awarded a contract for the development of the General Electric J85 and Fairchild was awarded a contract
XSM-73_Goose
Military training aircraft
Whitney JT12A-5 turbojet engine, this would be substituted for by a General Electric J85 powerplant for the subsequent production aircraft that followed.
Canadair_CT-114_Tutor
Kit-built supersonic aircraft
the General Electric J85, widely used in a variety of military aircraft and virtually identical to its civilian counterpart, the General Electric CJ610
Bede_BD-10
American military turbojet engine
development Pratt & Whitney T73 Comparable engines Fairchild J83 General Electric J85 Ishikawajima-Harima J3 Rolls-Royce RB.108 Rolls-Royce RB.145 Rolls-Royce
Pratt_&_Whitney_JT12
Aircraft takeoff and landing class
nozzle controls. The Republic Aviation AP-100 was a prototype VTOL 6x General Electric J85 turbojet-engined nuclear-capable strike fighter concept designed
V/STOL
Taiwanese multirole jet fighter
such as the General Electric F404 or the Pratt & Whitney F100 were not available to Taiwan. Both the General Electric J85 and General Electric J79 were considered
AIDC_F-CK-1_Ching-kuo
1959 anti-submarine helicopter family by Kaman
wings and a General Electric J85 turbojet engine in May 1968.[citation needed] UH-2C UH-2A and UH-2B helicopters fitted with two General Electric T58-GE-8B
Kaman_SH-2_Seasprite
Airbreathing jet engine designed to provide thrust by driving a fan
CF700 engine, with a 2.0 bypass ratio. This was derived from the General Electric J85/CJ610 turbojet 2,850 lbf (12,700 N) to power the larger Rockwell
Turbofan
Manufacturing company
Engines and other aircraft manufacturers: General Electric J79 General Electric J85-CAN-40 General Electric J-85-CAN-15 Rail Hawker-Siddeley Transportation
Hawker_Siddeley_Canada
Soviet aerobatic aircraft
airframes, fitted with a new wing center section supporting a single General Electric J85 turbojet engine in addition to the Vedeneyev M14P propeller engines
Yakovlev_Yak-55
Series of target drones
FIM-92 Stinger man-portable SAMs, refitting these drones with a General Electric J85-GE-7 turbojet of 10.9 kN (2,500 lbf) thrust which were salvaged from
Ryan_Firebee
of the P5M-3 under the designation P7M Submaster, introducing two General Electric J85 BLC gas generators, one in the rear of each outer engine nacelle
Martin_P7M_SubMaster
American experimental VTOL aircraft
standard. The two Pratt & Whitney JT12 engines were replaced with six General Electric J85 turbojets, four of these units acting as lift jets. This aircraft
Lockheed_XV-4_Hummingbird
Vertifan V/STOL research aircraft (known earlier as the VZ-11). Two General Electric J85-5 turbojets were used for propulsion in wing-borne flight. During
General_Electric_X353-5
Temporary diversion of an aircraft engine's thrust
Board of Canada. One of the modifications was the installation of a General Electric J85 turbojet in the fuselage with its exhaust direction controllable
Thrust_reversal
American turbojet engine
a thrust to weight ratio goal of 10:1. General Electric was awarded a contract for the development of the J85 and Fairchild was awarded a contract for
Fairchild_J83
American decoy cruise missile
encountered during testing resulted in McDonnell replacing the J85-GE-3 with the J85-GE-7 engine in the production GAM-72A. The GAM-72A was also about
ADM-20_Quail
Aircraft propulsion configuration with fans in a fixed wing
the 1960s. The Republic Aviation AP-100 was a prototype VTOL 6x General Electric J85 Turbojet engined nuclear capable strike fighter concept designed
Lift_fan
Canadian fighter aircraft introduced 1968
almost 20%. A midair refueling probe was installed, Orenda-built General Electric J85-15 engines with 4,300 lbf (19 kN) thrust were used, and a more sophisticated
Canadair_CF-5
Airport in New Brunswick, Canada
Limited, who own and operate the air tanker fleet. In addition, a General Electric J85 engine test facility is located at the airport. The airport is the
Miramichi_Airport
French light attack fighter
Alpha Jet. West Germany was interested in powering the type with the General Electric J85, but France objected to the use of an American engine which would
Dassault/Dornier_Alpha_Jet
Spanish engine manufacturer
for Airbus A400M Atlas transport aircraft. General Electric CT7-8F5 General Electric F414 General Electric J85-5-21 MTR MTR390-E (European consortium MTRI)
ITP_Aero
1959 experimental VTOL aircraft model
verticals — "winglets". Both designs used two 2,700 lbf (12 kN) thrust General Electric J85 turbojets and increased the turborotor diameter from five to six
Avro_Canada_VZ-9_Avrocar
Engine designed for use in powered aircraft
The last successful entry in the global market for jet engines was General Electric in the 1970s. These barriers to entry make the market very lucrative
Aircraft_engine
Experimental American aircraft design
370 lb (1,529 kg) Gross weight: 4,030 lb (1,828 kg) Powerplant: 1 × General Electric J85-GE-21 turbojet Performance Maximum speed: 1,218 mph (1,960 km/h,
Rockwell_HiMAT
History of development and use of UAVs
wedge-shaped stubby wings, swept conventional tail assembly, and a General Electric J85 turbojet engine, like that used on the Northrop F-5 fighter.[citation
History of unmanned aerial vehicles
History_of_unmanned_aerial_vehicles
Vehicle propelled by ejection of gases
Shuttle Max-Q". Aerospaceweb. 2001-05-06. Retrieved 2012-12-10. "General Electric J85". Geae.com. 2012-09-07. Archived from the original on 2011-07-22
Rocket
American business jet
[citation needed] Sabreliner (NA-265 or NA-246) Prototype powered by two General Electric J85-GE-X turbojet engines, one built sometimes unofficially called XT-39
North_American_Sabreliner
Italian jet fighter-bomber aircraft
replaced the original single Bristol Siddeley Orpheus engine with two General Electric J85 units in a "completely re-engineered structure" giving 60% more power
Fiat_G.91
1956 primary jet trainer aircraft family
The J69 was replaced with a 2,850 lbf (12.7 kN) General Electric CJ610 (the civil version of the J85). The modified aircraft, called the T-610 Super Pinto
Temco_TT_Pinto
Space tourism company
traveling at 2,335 km/h (1,451 mph). XB-1 would be equipped with General Electric J85 engines, Honeywell avionics, with composite structures fabricated
Virgin_Galactic
Supersonic drone
expendable turbojet, 1,810 lbf (8.1 kN) thrust Q-4B/AQM-35B: 1x General Electric J85-GE-5 turbojet, 3,850 lbf (17 kN) thrust Performance Service ceiling:
Northrop_AQM-35
J35 General Electric J39 General Electric J47 General Electric J53 General Electric J73 General Electric J77 General Electric J79 General Electric J85 General
List_of_aircraft_engines
- Reverse engineered Williams FJ33. IAIO Owj Reverse engineered General Electric J85. Toloue-4 Turbojet engine - Reverse engineered Microturbo TRI 60
List of military equipment manufactured in Iran
List_of_military_equipment_manufactured_in_Iran
Iranian defence company
this engine. It is a reverse-engineered and enhanced version of the General Electric J85 turbojet engine (expected to serve with U.S. Air Force until 2040
Iran Aviation Industries Organization
Iran_Aviation_Industries_Organization
Iranian jet trainer aircraft prototype (1991)
powerplant is disputed: some sources report a single non-afterburning General Electric J85 turbojet, but Taghvaee attributes this specific engine to the succeeding
HESA_Dorna
American aviator
inventor of the Shockwave jet truck, modified his Waco, attaching a General Electric J85 jet engine to the underside. It was in this aircraft that Franklin's
Jimmy_Franklin
American aviation inventor
selected the smallest production engine he could find in quantity, the General Electric J85, and designed an aircraft around it. The resulting design bore some
Jim_Bede
Car powered by an aircraft engine
Elaine Larsen and Marisha Falk both drove jet dragsters powered by General Electric J85 engines capable of producing 5,000 hp (3,700 kW). Although rare,
Aero-engined_car
Measurement indicator of fuel conversion
velocity, converts to head-on velocity as it strikes a stationary vane. General Electric J85 turbojet compressor showing the axial spacing between rotating and
Jet_engine_performance
Military unit
squadron received its first UC-123K, equipped with two additional General Electric J85 engines, which greatly reduced the planes' vulnerability to loss
12th Airborne Command and Control Squadron
12th_Airborne_Command_and_Control_Squadron
companies during the decade, and was the European distributor of the General Electric J85 and CJ610 turbojets. It was also involved, alongside FIAT, FN of
Alfa_Romeo_Avio
Polish aerospace engineer
Rudlicki constructed a controlled discharge nozzles for jet engine General Electric J85, allowing the engine thrust vector deflection for vertical take-off
Jerzy_Rudlicki
Canadian aerospace manufacturer
for commercial and defence aircraft manufacturers: General Electric - F101, F110, F404, F414, J79, J85, CF34, CF700, CJ610, LM2500, LM7000, CFE738, T64
Magellan_Aerospace
288 kg (2,840 lb) Gross weight: 2,645 kg (5,831 lb) Powerplant: 1 × General Electric J85-GE-5 turbojet, 13.01 kN (2,920 lbf) thrust Performance Maximum speed:
Venga_TG-10
Business jet
in Amsterdam, and Modane in France. The selection of the American General Electric CJ610 turbojet engine to power the design was a straightforward choice;
HFB_320_Hansa_Jet
South Korean Aerospace company
comprised the production and repair of jet engines, including assembly of the GE J85, CFM56, LM2500 and F404 engines as well as, in cooperation with Pratt & Whitney
Samsung_Aerospace
corrosion-resistant high-temperature coatings. Woll was a lead in developing the J85, CJ610, and CF700 engines which enabled lightweight jet fighters, such as
Ed_Woll
Type of continuous-flow turbine engine
submitted a thesis on gas turbines. In 1903, Moss became an engineer for General Electric's Steam Turbine Department in Lynn, Massachusetts. While there, he applied
Gas-turbine_engine
Nozzle that converts the internal energy of a working gas into propulsive force
fixed geometry cylindrical shroud surrounding the afterburning nozzle on the J85 installation in the T-38 Talon. More complex were the arrangements used for
Propelling_nozzle
Airbreathing jet engine which is typically used in aircraft
as a result of an extended 500-hour run being achieved in tests. General Electric in the United States was in a good position to enter the jet engine
Turbojet
City in Cowley County, Kansas
overhauling and repairing entire military jet engines (particularly J73 and J85), and related parts and accessories—ultimately processing over 6,000 jet
Winfield,_Kansas
American Aerospace Company
level test of F100, F101, F110, F119, F124, F125, F135, F404, F414, J79, J85, TF30, TF33, TF34, TFE731, T38, T53, T56, 501D, AE2100, PT6, CT7, TPE331
Atec
Observation and light attack aircraft
OV-10B(Z) when fitted with an additional J85-GE-4 turbojet. OV-10B(Z) A variation of the German target tug, with one J85-GE-4 turbojet mounted in a nacelle
North American Rockwell OV-10 Bronco
North_American_Rockwell_OV-10_Bronco
British "Big 4" railway company, active 1923–1947
during the General Strike, an express passenger train was deliberately derailed south of Cramlington, Northumberland. On 7 August 1926, an electric multiple
London and North Eastern Railway
London_and_North_Eastern_Railway
GCR railcar introduced in 1912
The GCR petrol-electric railcar, also informally known as the Bollington Bug, was a 2-bogied motorised coach purchased by the Great Central Railway in
GCR_petrol-electric_railcar
Aircraft engine that produces thrust by emitting a jet of gas
(de Havilland Ghost turbojet) in the 1950s to 115,000 lbf (510 kN) (General Electric GE90 turbofan) in the 1990s, and their reliability went from 40 in-flight
Jet_engine
Class of 15 British 4-6-2 locomotives
D29 D30 D31 D32 D33 D34 D35 D36 E7 J31 J32 J33 J34 J35 J36 J37 J81 J83 J84 J85 J86 J88 N14 N15 Y9 North Eastern A2 A6 A7 B13 B14 B15 B16 C6 C7 D17/1 D17/2
LNER_Peppercorn_Class_A2
On 28 December 1932, whilst the locomotive was in Doncaster Works for general repair, new nameplates were fitted reading Knight of Thistle, which was
List of LNER Class A1/A3 locomotives
List_of_LNER_Class_A1/A3_locomotives
Class of 70 British 2-6-0 locomotives
D29 D30 D31 D32 D33 D34 D35 D36 E7 J31 J32 J33 J34 J35 J36 J37 J81 J83 J84 J85 J86 J88 N14 N15 Y9 North Eastern A2 A6 A7 B13 B14 B15 B16 C6 C7 D17/1 D17/2
LNER Thompson/Peppercorn Class K1
LNER_Thompson/Peppercorn_Class_K1
British locomotive classification system
the constituent companies used only steam locomotives. The NER had 13 electric lomotives, numbered 1-13, but this was in fact in the company's main locomotive
LNER locomotive numbering and classification
LNER_locomotive_numbering_and_classification
Fuel efficiency of an engine design with respect to thrust output
aerodynamically efficient, i.e., the lift to drag ratio is far lower. In general, the total fuel burn of a complete aircraft is of far more importance to
Thrust-specific fuel consumption
Thrust-specific_fuel_consumption
Class of British steam locomotives
D29 D30 D31 D32 D33 D34 D35 D36 E7 J31 J32 J33 J34 J35 J36 J37 J81 J83 J84 J85 J86 J88 N14 N15 Y9 North Eastern A2 A6 A7 B13 B14 B15 B16 C6 C7 D17/1 D17/2
NBR_G_Class
Class of 184 three-cylinder 2-6-2 locomotives
D29 D30 D31 D32 D33 D34 D35 D36 E7 J31 J32 J33 J34 J35 J36 J37 J81 J83 J84 J85 J86 J88 N14 N15 Y9 North Eastern A2 A6 A7 B13 B14 B15 B16 C6 C7 D17/1 D17/2
LNER_Class_V2
Class of 289 two-cylinder locomotives
D29 D30 D31 D32 D33 D34 D35 D36 E7 J31 J32 J33 J34 J35 J36 J37 J81 J83 J84 J85 J86 J88 N14 N15 Y9 North Eastern A2 A6 A7 B13 B14 B15 B16 C6 C7 D17/1 D17/2
LNER_Class_J39
Class of small jet aircraft under 10,000 lb.
of their passengers. Despite this, the Eclipse 500 had the option of an electric flush, remove-to-service lavatory with a privacy curtain - at the expense
Very_light_jet
S-class submarine of the United States
2, at 20:09, the destroyer HNoMS St. Albans and minesweeper HMS Seagull (J85), attacked a submerged contact at 73°01′N 17°32′E / 73.017°N 17.533°E
USS_S-25
British steam locomotive class (built 1935)
8 km/h) and completed the journey in under four hours, the LNER's Chief General Manager Ralph Wedgwood authorised Gresley to produce a streamlined development
LNER_Class_A4
travel, tourism, insurance
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