05 Apr 2012, 22:23
At the link 'cola' provided the info is this: (under the 'characteristics' tab). 'TEG' will probably have an explanation whilst 'g3143' seems to be close, perhaps engine control software limits engine output for prolonging engine service life? Anyway:
Engine Characteristics
Conventional Take Off and Landing CTOL / CV Engine Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Intermediate Thrust (in pounds): 28,000 (128.1 kN)
Length: 220 inches (5.59 meters)
Inlet Diameter: 46 inches (1.17 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio: 0.57 Overall Pressure Ratio: 28
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Short Take Off and Vertical Landing STOVL Propulsion System Design
Maximum Thrust (in pounds): 43,000 (191.3 kN)
Short Takeoff Thrust: 38,100 (169.5 kN)
Hover Thrust: 39,400 (175.3 kN)
Main Engine: 15,700
Lift Fan: 20,000
Roll Post: 3,700
Length
Main Engine: 369 inches (9.37 meters)
Inlet Diameter: 46 inches (1.17 meters)
Lift Fan: 50 inches (1.27 meters)
Maximum Diameter: 51 inches (1.30 meters)
Bypass Ratio
Conventional: 0.56
Powered Lift: 0.51
Overall Pressure Ratio
Conventional: 28
Powered Lift: 29
A4G Skyhawk: www.faaaa.asn.au/spazsinbad-a4g/ & www.youtube.com/channel/UCwqC_s6gcCVvG7NOge3qfAQ/videos?view_as=subscriber