• 3/6/18 5:22 am
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I finished this jet a little while after finishing the RAF pack but I never got around uploading it. Now is the time.
General characteristics
Performance
Armament
General characteristics
- Crew: 1
- Length: 15.35 m (50 ft 4 in)
- Wingspan: 9.42 m (30 ft 10 in)
- Height: 3.89 m (12 ft 9 in)
- Wing area: 49.20 m² (529.6 ft²)
- Empty weight: 7,865 kg (17,340 lb)
- Loaded weight: 11,000 kg (24,250 lb)
- Max. takeoff weight: 16,000 kg (35,273 lb)
- Powerplant: 1 × Volvo Flygmotor RM6C afterburning turbojet
- Dry thrust: 56.5 kN (12,787 lbf)
- Thrust with afterburner: 78.4 kN (17,637 lbf)
- Dry thrust: 56.5 kN (12,787 lbf)
Performance
- Maximum speed: Mach 2.0 (1990s improvements)
- Range: 2,750 km (1,709 mi) with external drop tanks
- Service ceiling: 20,000 m (65,600 ft)
- Rate of climb: 250 m/s (49,200 ft/min)
- Wing loading: 231.6 kg/m² (47.4 lb/ft²)
- Thrust/weight: 0.70
- Takeoff roll: 800 m (2,623 ft)
Armament
- Guns: 1× or 2× 30 mm M-55 ADEN cannon with 100 rounds per gun (in Saab 35F one cannon was omitted to fit avionics needed for Falcon missile integration, earlier variants and export variants retained twin guns.)
- Hardpoints: for fuel tanks or ordnance with a capacity of 2,900 kg (6,393 lb) and provisions to carry combinations of:
- Rockets: 2× 75 mm air-to-ground rocket pods ventrally or 12× 135 mm rockets on six underwing pylons
- Missiles: Rb 24, Rb 27 and Rb 28 air-to-air missiles
- Bombs: The Danish export version, (F-35), was modified according to NATO standards and was fitted with 1,000lb bomb hardpoints
- Rockets: 2× 75 mm air-to-ground rocket pods ventrally or 12× 135 mm rockets on six underwing pylons
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