m13katyusa2020
Senior Airman
- 472
- Mar 26, 2022
Rolls-Royce Spey were used on TRIDENT Jets, and Spey MK202 Turbofan jet is a jet used on F-4K English edition, which lengthened the range of F-4K, and enhanced F-4K's low speed and altitude performance.
General specs:
Type: Low bypass turbofan
Length: 204.9 in (5204.4 mm)
Diameter: 43.0 in (1092.2 mm)
Dry weight: 4,093 lb (1856 kg)
Compressor: axial flow, 5-stage LP, 12-stage HP
Combustors: 10 can-annular combustion chambers
Turbine: 2-stage LP, 2-stage HP
Maximum thrust: Dry thrust: 12,140 lbf (54 kN); with reheat: 20,500 lbf (91.2 kN)
Air mass flow: 204lb/sec (92.53 kg/s)
Specific fuel consumption: 1.95 lb/(lbf·h) with afterburner, 0.63 lb/(lbf·h) at military thrust Engines on display Specifications (Spey Mk 202)
Thrust-to-weight ratio: 5:1
The manuals are separated in many parts, and the first post of the manual is performance manual, maintenance manual, as well as the parts numerial index of Spey Mk202.
Addon: Retired Spey engine training course note:
alternate link:
another alternate link with access code 1234
Disclaimer: These items are shared for reference, sharing for non-profitable use only.
This manuals and blueprints are not meant to be used for current update material for certification / repair, but make an excellent reference for the scholar, collector, modeler or aircraft buffs .... For proprietary reasons we generally only provide civil manuals and blueprints on obsolete Aircraft / Engines / Helicopter. The information is for reference only and we do not guarantee the accuracy or currency of any manuals.
Reference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.
Please download the following 3 pdf attachments:
General specs:
Type: Low bypass turbofan
Length: 204.9 in (5204.4 mm)
Diameter: 43.0 in (1092.2 mm)
Dry weight: 4,093 lb (1856 kg)
Compressor: axial flow, 5-stage LP, 12-stage HP
Combustors: 10 can-annular combustion chambers
Turbine: 2-stage LP, 2-stage HP
Maximum thrust: Dry thrust: 12,140 lbf (54 kN); with reheat: 20,500 lbf (91.2 kN)
Air mass flow: 204lb/sec (92.53 kg/s)
Specific fuel consumption: 1.95 lb/(lbf·h) with afterburner, 0.63 lb/(lbf·h) at military thrust Engines on display Specifications (Spey Mk 202)
Thrust-to-weight ratio: 5:1
The manuals are separated in many parts, and the first post of the manual is performance manual, maintenance manual, as well as the parts numerial index of Spey Mk202.
Addon: Retired Spey engine training course note:
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another alternate link with access code 1234
Disclaimer: These items are shared for reference, sharing for non-profitable use only.
This manuals and blueprints are not meant to be used for current update material for certification / repair, but make an excellent reference for the scholar, collector, modeler or aircraft buffs .... For proprietary reasons we generally only provide civil manuals and blueprints on obsolete Aircraft / Engines / Helicopter. The information is for reference only and we do not guarantee the accuracy or currency of any manuals.
Reference herein to any specific commercial products by trade name, trademark, manufacturer, or otherwise, is not meant to imply or suggest any endorsement by, or affiliation with that manufacturer or supplier. All trade names, trademarks and manufacturer names are the property of their respective owners.
Please download the following 3 pdf attachments:
Attachments
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