Specifications (G.91R)
General characteristics
- Crew: 1
- Length: 10.3 m (33 ft 9 in)
- Wingspan: 8.56 m (28 ft 1 in)
- Height: 4.0 m (13 ft 1 in)
- Wing area: 16.4 m² (177 ft²)
- Empty weight: 3,100 kg (6,830 lb)
- Loaded weight: 5,440 kg (11,990 lb)
- Max. takeoff weight: 5,500 kg (12,100 lb)
- Powerplant: 1 × Bristol Siddeley Orpheus 803 turbojet, 22.2 kN (5,000 lbf)
Performance
- Maximum speed: 1,075 km/h (580 kn, 668 mph)
- Range: 1,150 km (621 nmi, 715 mi)
- Service ceiling: 13,100 m (43,000 ft)
- Rate of climb: 30 m/s (6,000 ft/min)
- Wing loading: 331 kg/m² (67.8 lb/ft²)
- Thrust/weight: 0.42
Armament
- Guns:
4× 12.7 mm (0.50 in) M2 Browning machine guns; or
2× 30 mm (1.18 in) DEFA cannons (Luftwaffe G.91R/3 only) - Hardpoints : 4× under-wing pylon stations holding up to maximum of 1,814 kg/4,000 lb of payload for G.91Y, 680 kg/1,500 lb for G.91R/3 & R/4 and 500 kg/1,100 lb for G.91R/1
- Rockets:
2× Matra rocket pods (each with 19× SNEB 68 mm rockets); or
18× Hispano SURA R80 80 mm rockets - Bombs: A wide variety of air-to-ground ordnance including unguided iron bombs, gun pods in addition to auxiliary drop tanks for extended range
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