Variants
Note:'
- Sabre I (E.107)
- (1939) 2,000 horsepower (1,490 kW).
- Sabre II
- (1940) 2,300 horsepower (1,715 kW). Experimental 0.332:1 propeller reduction gear ratio.
- Sabre II (production variant)
- 2,200 horsepower (1,640 kW). Reduction gear ratio 0.274:1: mainly used in early Hawker Typhoons.
- Sabre IIA
- 2,235 horsepower (1,665 kW). Revised ignition system: maximum boost +9 lbs.
- Sabre IIB
- 2,400 horsepower (1,790 kW). Four choke S.U. carburettor: Mainly used in Hawker Tempest V.
- Sabre IIC
- 2,065 horsepower (1,540 kW). Similar to Mk VII.
- Sabre III
- 2,250 horsepower (1,680 kW). Similar to Mk IIA, tailored for the Blackburn Firebrand: 25 manufactured and installed.
- Sabre IV
- 2,240 horsepower (1,670 kW). As Mk VA with Hobson fuel injection: preliminary flight development engine for Sabre V series. Used in Hawker Tempest I.
- Sabre V
- 2,600 horsepower (1,940 kW). Developed MK II, redesigned supercharger with increased boost, redesigned induction system.
- Sabre VA
- 2,600 horsepower (1,940 kW). Mk V with Hobson-R.A.E fuel injection, single-lever throttle and propeller control: used in Hawker Tempest VI.
- Sabre VI
- 2,310 horsepower (1,720 kW). Mk VA with Rotol cooling fan: used in 2 Hawker Tempest Vs modified to use Napier designed annular radiators; also in experimental Vickers Warwick V.
- Sabre VII
- 3,055 horsepower (2,278 kW). Mk VA strengthened to withstand high powers produced using Water/Methanol injection. Larger supercharger impeller.
- Sabre VIII
- 3,000 horsepower (2,240 kW). Intended for Hawker Fury; tested in the Folland Fo.108.
- Sabre E.118
- (1941) Three-speed, two-stage supercharger, contra-rotating propeller; test flown in Fo.108.
- Sabre E.122
- (1946) 3,500 horsepower. Intended for Napier 500mph tailless fighter
Read more about this topic: Napier Sabre
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