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Title: Aero-Engine Emporium
Description: Your one-stop shop for aero-engines


Juumanistra - May 14, 2008 08:35 PM (GMT)
Fairly simple stuff, methinks. Components ahoy!

Juumanistra - May 14, 2008 08:39 PM (GMT)
TW-HPM-S145/170 Aspirant
Primary Contractor: Tachibana-WrATUR Aero-Engine Union
Length: 5.95m
Diameter: 1.12m(fan diameter); Variable intake diameter, depending upon the aircraft in question
Dry Weight: 2,152kg
Components:
-Configuration: Double spooled variable post-compression bypass turbofan
-Compressor: Axial compressor with four fans and ten compressor stages
-Turbine: One low-pressure stage and one high-pressure stage
Bypass Ratio: Variable
Pressure Ratio: 36:1
Maximum Thrust, Dry: ~14,500kgf, ~142kN
Maximum Thrust, Wet: ~17,000kgf, ~167kN
Thrust-to-Weight Ratio, Dry: ~6.73:1 kgf/kg, ~65.99:1 N/kg
Thrust-to-Weight Ratio, Wet: ~7.90:1 kgf/kg, ~77.60:1 N/kg
Utilized By: Na-24G Block 15/VIII Mako
Cost:
-New Unit Price: ][6,000,000 [~$12,000,000]
-New Unit Export Price: ][7,500,000 [~$15,000,000]

Juumanistra - May 15, 2008 07:40 PM (GMT)
D&W-G2M-T108/167
Primary Contractor: Davidson & Williams Turbineers, Ltd.
Length: 4.09m
Diameter: 0.912m(fan diameter); Variable intake diameter, depending upon the aircraft in question
Dry Weight: 1,836kg
Components:
-Configuration: Double spooled low bypass turbofan
-Compressor: Axial compressor with four fans and eight compressor stages
-Turbine: Two low-pressure stages and one high-pressure stage
Bypass Ratio: 0.32:1
Pressure Ratio: 33:1
Maximum Thrust, Dry: ~11,500kgf, ~113kN
Maximum Thrust, Wet: ~16,000kgf, ~157kN
Thrust-to-Weight Ratio, Dry: ~6.26:1 kgf/kg, ~61.54:1 N/kg
Thrust-to-Weight Ratio, Wet: ~8.71:1 kgf/kg, ~85.51:1 N/kg
Utilized By: Ni-35FX Tsunami
Cost:
-New Unit Price: ][3,200,000 [~$6,400,000]
-New Unit Export Price: ][3,800,000 [~$7,600,000]




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