Aeronautic Engines Data
|
| Engine | Aircraft | T | pr | BPR | SFC | T/W | Notes |
|---|---|---|---|---|---|---|---|
| GE CF6-50A | A-300 | 245 | 31.5 | 4.4 | 6.6 | 5.92 | . |
| PW JT9D-3A | B 747/100 | 190 | 21.4 | 5.2 | 3.6 | 5.05 | . |
| RR RB211-524 | L-1011 | 220 | 10.8 | 1.02 | 6.4 | 5.00 | . |
| Kuznetzov NK-144 | Tu 144 | 196 | 27.0 | 5.0 | 7.8 | 5.85 | w/ afterburning |
| Snecma/RR Olympus 593 | Concorde | 170 | . | . | 120 | . | w/ afterburning |
| PW JT4A-3 | B707-300 | 70.3 | . | . | 0.780 | 3.15 | . |
| Engine | Type | BPR | T/W | T | pr | Ma | SFC | Notes |
|---|---|---|---|---|---|---|---|---|
| RR Spey I | turbofan | 1.02 | 1.43 | 43.81 | 16.75 | 91.5 | 0.787 | 32k ft, 508 kt |
| RR Conway Rco.12 | turbofan | 0.3 | 1.05 | 80.06 | 14.10 | 127.3 | 0.9 | 35k ft, 475 kt |
| RR Avon RA.29/6 | turbofan | . | 1.34 | 56.60 | 10.3 | 83.8 | 0.918 | 25k ft, 425 kt |
| PW JT3D-1 | turbofan | 1.4 | 0.78 | 75.62 | 12.5 | 217.4 | 0.8 | 20k ft, 525 kt |
| PW JT3C-26 | turbojet | . | . | 80.06 | 12.5 | 81.5 | . | . |
| GE CJ805-23A | aft-fan | 1.56 | 1.37 | 71.61 | 13.0 | 76.1 | 0.83 | 25k ft, 525 kt |
| Allison T63-I | t-prop | . | . | . | 6.2 | 1.4 | 0.72 | 6k ft, 200 kt |
Nomenclature
| BPR | = | by-pass ratio |
| Ma | = | total air mass flow (kg/s) |
| pr | = | compression ratio |
| P | = | maximum power (kN) |
| SFC | = | specific fuel consumption (kg/kN h) |
| T | = | thrust (kN) |
| W | = | dry weight (kg) |
| T/W | = | thrust-to dry weight at cruise, as noted |
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A. Filippone (1999-2004). All Rights Reserved.
