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Military Jet Engine Acquisition Technology Basics and Cost-Estimating Methodology

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Military Jet Engine Acquisition Technology Basics and Cost-Estimating Methodology ( military-jet-engine-acquisition-technology-basics-and-cost-e )

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68 Military Jet Engine Acquisition Engine Rating Point) Consump- sure (kg/second) tion Ratio 20,300 0.80 24.0 (Fo) Ratio second) (lbs) No=0) Contract Award Nov 1988 Oct 1962 Oct 1966 May 1969 N/A Sep 1987 Nov 1975 Mar 1985 F120GE-100 Pegasus 5 Pegasus 6 F402RR-401 F402RR-406 F402RR-408 F404GE-400 F404GE - 15,500 0.63 13.7 19,000 0.64 13.8 20,500 0.65 14.7 21,500 0.66 14.7 23,390 0.75 15.5 10,600 0.81 24.0 10,800 0.82 25.0 3,000 8.13 275 1,990 4.59 394 2,160 5.29 409 2,215 5.51 409 2,260 5.70 437 2,467 6.00 459 2,459 7.48 140 2,534 6.02 142 4,000 1 3,380 0 3,591 0 3,720 0 3,770 0 3,900 0 2,140 1 1,795 0 400D F404GE - RM12 11,500 0.70 26.0 2,535 7.79 150 2,310 1 5,250 Dec 1987 Jun 1981 F414GE-400 JT8D-9 JT9D-3 JT9D-7 F105PW- 14,327 0.84 27.2 14,500 0.60 15.9 43,600 0.37 21.5 45,600 0.36 22.3 45,600 0.36 22.3 2,757 8.68 174 1,720 4.46 318 2,300 4.93 1,510 2,350 5.15 1,535 2,405 5.15 1,535 2,445 1 3,252 0 8,850 0 8,850 0 8,850 0 10,463 6,067 4,800 13,100 N/A Nov 1996 Jan 1963 Jan 1970 Jun 1971 Jun 1971 N/A Mar 1960 Jun 1966 N/A Aug 1967 Thrust (at Specific Overall Intermediate Fuel Pres- Rotor Inlet Thrust- Air Temper- to- Flow ature Weight (lbs/ After- Dry burner Weight (Yes=1/ Full- Scale Test Hours 13,905 4,000 6,500 5700 8,300 2,301 14,900 11,400 Low-Rate Produc- tion Release Jan 1993 Oct 1964 Oct 1968 Jun 1971 N/A N/A Jun 1979 N/A Table 6.2—Continued 100 JT9D-59A JT9D-7Q JT9D-7R4D NOTES: Air flow = The rate of airflow through an engine, measured in pounds of air per second; AF = U.S. Air Force; N = U.S. Navy; USMC = U.S. Marine Corps; C = Commercial; N/A = Not available. 53,000 0.37 24.5 53,000 0.37 24.5 48,000 0.34 23.0 2,400 5.99 1,640 2,400 5.70 1,640 2,320 5.39 1,575 8,850 0 9,295 0 8,905 0 23,600 22,500 14,300 Dec 1974 Oct 1978 Nov 1980 N/A N/A N/A Utopia R ✺❁❐❆

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