| 词条 | General Electric J97 | ||||||||||||||
| 释义 |
The General Electric J97 is a single-shaft turbojet engine designed and built by General Electric as a compact high-performance engine for light attack fighters and eventually a number of drone projects. Development and designThe J97 was based on GE's General Electric GE1/J1 series of turbojets and the engine development was financed by the United States Air Force.[1] The original application was to be the Northrop P-530 (which later evolved into the YF-17), but it was ultimately only used in several small drone aircraft. Variants
Applications
Specifications (J97-GE-100){{jetspecs|ref=[4] |type=Turbojet engine |length= 109.5in (2.78m) |diameter= 24.4in (0.62m) |weight=694lb (315kg) |compressor= 14-stage |combustion= annular |turbine= two-stage |fueltype= |oilsystem= |power= |thrust= Take-off 5,270lb (23.4kN) dry, 8,000lbf (35kN) afterburner |compression= |aircon= |turbinetemp= |fuelcon= |specfuelcon= |power/weight= |thrust/weight= 11.5:1 }} See also{{Aircontent|related= |similar engines= |lists=
|see also= }} References1. ^1 {{Cite magazine |title=Turbine Engines of the World |magazine=FLIGHT International |date=4 January 1973 |page=34 |url=http://www.flightglobal.com/pdfarchive/view/1973/1973%20-%200043.html}} [1][2][3]2. ^1 {{Cite magazine |title=For the executive in a hurry |magazine=FLIGHT International |date=5 June 1976 |page=1488 |url=https://www.flightglobal.com/pdfarchive/view/1976/1976%20-%200950.html}} 3. ^1 {{Cite magazine |title=J97 |department=International Turbine Engine Directory |magazine=FLIGHT International |date=7 January 1978 |page=44 |url=https://www.flightglobal.com/pdfarchive/view/1978/1978%20-%200036.html}} }}{{GE aeroengines}}{{USAF gas turbine engines}} 3 : Turbojet engines 1960–1969|General Electric aircraft engines|Abandoned military aircraft engine projects of the United States |
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