Fairchild J44

Last updated
J44
Frontiers of Flight Museum December 2015 077 (Fairchild J44R-24 jet engine).jpg
A Fairchild J44R-24 on display at the Frontiers of Flight Museum
Type Turbojet
National origin United States
Manufacturer Fairchild Engine Division
First runAugust 1948
Major applications Ryan AQM-34 Firebee
C-123 Provider
Developed into Fairchild J83

The Fairchild J44 was a small turbojet developed in the 1940s by the Fairchild Engine Division.

Contents

Design and development

The Fairchild Engine Division (previously the Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation) began development of the J44 in 1947. It was used in target drones, missiles, and as jet boosters on several aircraft types.

Applications

Variants

Data from: Aircraft engines of the World 1953, [1] Flight 20 March 1959 :AERO ENGINES 1959 . . ., [2] Aircraft engines of the World 1957 [3]

XJ44
Prototypes of the J44
J44-R-1
United States Air Force (USAF) engine, similar to the United States Navy (USN) -6, 950 lbf (4.2 kN).
J44-R-2
Same as -6 but with different installation.
J44-R-3
Longer life - Fairchild C-123 Provider wing-tip boosters.
J44-R-6
USN version, 950 lbf (4.2 kN).
J44-R-12
expendable.
J44-R-20B
Ryan Firebee.
J44-R-24
Fairchild Petrel.
J44-R-26
1,100 lbf (4.9 kN) company sponsored variant.
FT-101E
Commercial version of -3.
FT-101-G
Commercial version with return oil system.

Specifications(J44-R-3)

Data from Jane's all the World's Aircraft 1955-56, [4] Minijets: Fairchild J44, [5] Turbojet History and Development 1930-1960 Volume 2, [6] Aircraft engines of the World 1957 [3]

General characteristics

Components

Performance

See also

Related development

Related lists

Related Research Articles

<span class="mw-page-title-main">Pratt & Whitney J57</span> Turbojet engine

The Pratt & Whitney J57 is an axial-flow turbojet engine developed by Pratt & Whitney in the early 1950s. The J57 was the first 10,000 lbf (45 kN) thrust class engine in the United States. The J57/JT3C was developed into the J52 turbojet, the J75/JT4A turbojet, the JT3D/TF33 turbofan, and the XT57 turboprop. The J57 and JT3C saw extensive use on fighter jets, jetliners, and bombers for many decades.

<span class="mw-page-title-main">Pratt & Whitney J75</span> Turbojet engine

The Pratt & Whitney J75 is an axial-flow turbojet engine first flown in 1955. A two-spool design in the 17,000 lbf (76 kN) thrust class, the J75 was essentially the bigger brother of the Pratt & Whitney J57 (JT3C). It was known in civilian service as the JT4A, and in a variety of stationary roles as the GG4 and FT4.

<span class="mw-page-title-main">Allison J35</span>

The General Electric/Allison J35 was the United States Air Force's first axial-flow compressor jet engine. Originally developed by General Electric in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN).

<span class="mw-page-title-main">Snecma Atar</span> Turbojet aircraft engine

The Snecma Atar is a French axial-flow turbojet engine built by Snecma. It was derived from the German World War II BMW 018 design, and developed by ex-BMW engineers through a progression of more powerful models. The name is derived from its original design group, Atelier technique aéronautique de Rickenbach near Lindau within the French Occupation Zone of Germany. The Atar powered many of the French post-war jet aircraft, including the Vautour, Étendard and Super Étendard, Super Mystère and several models of the Mirage.

<span class="mw-page-title-main">Allison J33</span>

The General Electric/Allison J33 is an American centrifugal-flow jet engine, a development of the General Electric J31, enlarged to produce significantly greater thrust, starting at 4,000 lbf (18 kN) and ending at 4,600 lbf (20 kN) with an additional low-altitude boost to 5,400 lbf (24 kN) with water-alcohol injection.

<span class="mw-page-title-main">Armstrong Siddeley Adder</span> 1940s British turbojet aircraft engine

The Armstrong Siddeley ASA.1 Adder was an early British turbojet engine developed by the Armstrong Siddeley company and first run in November 1948.

<span class="mw-page-title-main">Ryan Firebee</span> Series of target drones

The Ryan Firebee is a series of target drones developed by the Ryan Aeronautical Company beginning in 1951. It was one of the first jet-propelled drones, and remains one of the most widely used target drones ever built.

<span class="mw-page-title-main">Turbomeca Marboré</span>

The Turbomeca Marboré is a small turbojet engine that was produced by Turbomeca from the 1950s into the 1970s. The most popular uses of this engine were in the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris. It was also licensed for production in the United States as the Teledyne CAE J69.

<span class="mw-page-title-main">Allison J71</span>

The Allison J71 was a single spool turbojet engine, designed and built in the United States. It began development in 1948 as a much modified J35, originally designated J35-A-23.

<span class="mw-page-title-main">Pratt & Whitney JT12</span>

The Pratt & Whitney JT12, is a small turbojet engine. The Pratt & Whitney T73 is a related turboshaft engine.

The Fairchild J83 turbojet was developed starting in 1955 to power cruise missiles used as un-armed decoys for bomber aircraft. The engine's development was terminated in November 1958.

<span class="mw-page-title-main">General Electric YJ93</span>

The General Electric YJ93 turbojet engine was designed as the powerplant for both the North American XB-70 Valkyrie bomber and the North American XF-108 Rapier interceptor. The YJ93 was a single-shaft axial-flow turbojet with a variable-stator compressor and a fully variable convergent/divergent exhaust nozzle. The maximum sea-level thrust was 28,800 lbf (128 kN).

<span class="mw-page-title-main">Westinghouse J30</span> American pioneering jet aircraft engine

The Westinghouse J30, initially known as the Westinghouse 19XB, was a turbojet engine developed by Westinghouse Electric Corporation. It was the first American-designed turbojet to run, and only the second axial-flow turbojet to run outside Germany.

<span class="mw-page-title-main">General Electric J73</span> 1950s American turbojet engine

The General Electric J73 turbojet was developed by General Electric from the earlier J47 engine. Its original USAF designation was J47-21, but with innovative features including variable inlet guide vanes, double-shell combustor case, and 50% greater airflow was redesignated J73. Its only operational use was in the North American F-86H.

<span class="mw-page-title-main">Teledyne CAE J69</span> Turbojet aircraft engine series

The Teledyne CAE J69 was a small turbojet engine originally produced by Continental Aviation and Engineering (CAE) under license from Turbomeca. The J69 was a development of the Turbomeca Marboré II. It powered a number of U.S. drones, missiles and small aircraft. The engine was later produced by Teledyne CAE. The J69 was also developed into the Teledyne CAE J100 turbojet optimized for operation at higher altitudes.

The Flader J55, also known as the 124 within the company, was a small turbojet engine notable for its use of a supersonic axial-flow compressor. Development started at Fredric Flader Inc. in 1947, with the first examples being delivered in 1949. However, these delivered far lower power than predicted. Improved models followed in early 1952 that met the performance requirements, but demonstrated very poor reliability. When small engines from other companies became available, the J55 project was cancelled in 1952.

<span class="mw-page-title-main">Ishikawajima-Harima J3</span> 1960s Japanese turbojet aircraft engine

The Ishikawajima-Harima J3 was a Japanese turbojet aircraft engine. It was the first jet engine designed and built in Japan after the Second World War and was used to power the Fuji T-1 trainer and as a booster engine in the Kawasaki P-2J patrol aircraft.

The Turbomeca Piméné was a small French turbojet engine produced by Turbomeca in the early 1950s.

The Turbomeca Aspin was a small French turbofan engine produced by Turbomeca in the early 1950s. This geared turbofan design was the first turbofan to fly, powering the Fouga Gemeaux test-bed aircraft on 2 January 1952.

The Turbomeca Orédon was a small French turbo-shaft / Auxiliary Power Unit (APU) engine produced by Turbomeca in the late 1940s.

References

  1. Wilkinson, Paul H. (1953). Aircraft engines of the World 1953 (11th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 46.
  2. "AERO ENGINES 1959 . . . :Fairchild". Flight. 75 (2617): 404. 20 March 1959. Retrieved 7 January 2019.
  3. 1 2 Wilkinson, Paul H. (1957). Aircraft engines of the World 1957 (15th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 64.
  4. Bridgman, Leonard (1955). Jane's all the World's Aircraft 1955-56. London: Jane's all the World's Aircraft Publishing Co. Ltd.
  5. "Fairchild J44". Minijets (in French). Retrieved 7 January 2019.
  6. Kay, Anthony L. (2007). Turbojet History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary. Vol. 2 (1st ed.). Ramsbury: The Crowood Press. pp. 151–152. ISBN   978-1-86126-939-3.

Further reading