Variants
- 593 - Original version designed for Concorde
- Thrust : 20,000 lbf (89 kN) dry / 30,610 lbf (136 kN) reheat
- 593-22R - Powerplant fitted to prototypes. Higher performance than original engine due to changes in aircraft specification.
- Thrust : 34,650 lbf (154 kN) dry / 37,180 lbf (165 kN) reheat
- 593-610-14-28 - Final version fitted to production Concorde
- Thrust : 32,000 lbf (142 kN) dry / 38,050 lbf (169 kN) reheat
Read more about this topic: Rolls-Royce/Snecma Olympus 593
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