Avia S-105

1st Flight 1952
Aero S-105
Aero S-105
Czechoslovak licensed built MiG-19S by Aero Vodochody.
103 were built between 1958 and 1962.
Aero S-105
Specifications-
Crew: 1
Length: 12.54 m (41 ft 2 in) with pitot probe retracted; 14.64 m (48.0 ft) with pitot probe extended
Wingspan: 9 m (29 ft 6 in)
Height: 3.88 m (12 ft 9 in)
Wing area: 25 m2 (270 sq ft)
Airfoil: root: TsAGI SR-12S (8.74%); tip: TsAGI SR-7S (8%)
Empty weight: 5,172 kg (11,402 lb)
Gross weight: 7,560 kg (16,667 lb)
Max takeoff weight: 8,832 kg (19,471 lb) with 2 × 760 l (170 imp gal; 200 US gal) drop tanks and two rocket pods
Fuel capacity: 1,800 l (480 US gal; 400 imp gal) internal
Power plant: 2 × Tumansky RD-9B afterburning turbojet engines, 25.5 kN (5,700 lbf) thrust each dry, 31.8 kN (7,100 lbf) with afterburner
Aero S-105
Performance
Maximum speed: 1,452 km/h (902 mph, 784 kn) at 10,000 m (33,000 ft)
Maximum speed: Mach 1.35
Range: 1,390 km (860 mi, 750 nmi)
Ferry range: 2,200 km (1,400 mi, 1,200 nmi) with 2 × 760 l (200 US gal; 170 imp gal) drop tanks at 14,000 m (46,000 ft)
Service ceiling: 17,500 m (57,400 ft)
Rate of climb: 177.8 m/s (35,000 ft/min)
Armament
Guns: 3 × 30 mm Nudelman-Rikhter NR-30 auto cannon (75 rounds for wing-root guns, 55 rounds for the fuselage gun)
Hard points: 4 pylons in total, 2 for drop fuel tanks only, 2 for weapons, with a capacity of up to 500 kg (1,100 lb) of stores with provisions to carry combinations of:
Rockets: 2 × 32-round ORO-57K rocket pods (4 from 1957)
Bombs: 2 x FAB-250
Aero S-105
Credits-
AVIA, The Aviation Collection-Antonín Vlasák II
The Complete Book of Fighters-William Green & Gordon Swanborough
Wikipedia.

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