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Zhanrae30 — FD Scale Su-30SM

Published: 2018-05-02 09:25:51 +0000 UTC; Views: 1915; Favourites: 18; Downloads: 15
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Description A remaster and re-upload from Photobucket. Base Flanker courtesy of gollevainen, with some enhancements made by llamaman and kike-92

The Sukhoi Su-30 (Russian: Сухой Су-30; NATO reporting name: Flanker-C) is a twin-engine, two-seat supermaneuverable fighter aircraft developed by Russia's Sukhoi Aviation Corporation. It is a multirole fighter for all-weather, air-to-air and air-to-surface deep interdiction missions. The Su-30SM is a specialised version of the thrust-vectoring Su-30MKI and MKM variants for the Russian military, produced by the Irkut Corporation.Russia's Defence Ministry was impressed with the MKI's performance envelope and ordered 30 Su-30SMs, a localised version of Su-30MKI, for the Russian Air Force. The Su-30SM is considered as 4+ gen jet fighter. The new version has been upgraded based on Russian military requirements for radar, radio communications systems, friend-or-foe identification system, ejection seats, weapons, and other aircraft systems. The aircraft is equipped with the Bars-R radar and the wide-angle HUD. A contract for 60 of the multirole fighter was signed in March 2012 with delivery by 2016. On 21 September 2012 Su-30SM performed its maiden flight.Multirole Su-30SM fighter jet was accepted into service of the Russian Aerospace Forces by a resolution of the Russian president of January 12, 2018.

GENERAL CHARACTERISTICS


    Crew: 2
    Length: 21.935 m (73 ft)
    Wingspan: 14.7 m (48 ft 3 in)
    Height: 6.36 m (20 ft 10 in)
    Wing area: 62 m² (667 ft²)
    Empty weight: 17,700 kg (39,021 lb)
    Loaded weight: 24,900 kg (54,900 lb) with 56% fuel
    Max. takeoff weight: 34,500 kg (76,060 lb)
    Fuel capacity: 9,400 kg (20,724 lb) internally[105]
    Powerplant: 2 × Saturn AL-31FL turbofans
        Dry thrust: 74.5 kN (16,750 lbf) each
        Thrust with afterburner: 122.58 kN (27,560 lbf) each

PERFORMANCE

    Maximum speed: Mach 2.0 (2,120 km/h; 1,320 mph) at altitude
    Range: 3,000 km (1,860 mi; 1,620 nmi) at altitude
    Service ceiling: 17,300 m (56,800 ft)
    Rate of climb: 230 m/s (45,275 ft/min)
    Wing loading:
        With 56% fuel: 401 kg/m² (82.3 lb/ft²)
        With full internal fuel: 468.3 kg/m² ()
    Thrust/weight:
        With full fuel: 0.86
        With 56% fuel: 1
    Maximum g-load: +9 g

ARMAMENT

    Guns: 1 × 30 mm Gryazev-Shipunov GSh-301 autocannon with 150 rounds
    Hardpoints: 12 hardpoints with a capacity of up to 8,000 kg (18,000 lb) and provisions to carry combinations of:
        Rockets:
            S-8KOM/BM/OM
            S-13T/OF
            S-25OFM-PU
        Missiles:
            Air-to-air missiles:
                R-27R/ER/T/ET/P
                R-73E
                RVV-AE
            Air-to-surface missiles:
                Kh-29T/L
                Kh-59M/ME
            Anti-ship missiles:
                Kh-31A
            Anti-radiation missiles:
                Kh-31P
        Bombs:
            KAB-500KR general-purpose bomb
            KAB-500OD bomb
            KAB-1500KR GP bomb
            KAB-1500L laser-guided bomb
            FAB-500T GP bomb
            BETAB-500SHP bomb
            ODAB-500PM bomb
            OFAB-250-270 bomb
            OFAB-100-120 bomb
            P-50T bomb
            RBK-500 cluster bombs
            SPBE-D bomb

AVIONICS

    Bars planar array radar
    OEPS-27 electro-optical targeting system
    SPO-15 Radar Warning Receiver
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