Sukhoi Su-35BM (Multi-purpose)
- Crew: 1
- Length: 21.9 m (72.9 ft)
- Wingspan: 15.3 m (50.2 ft)
- Height: 5.90 m (19.4 ft)
- Wing area: 62.0 m² (667 ft²)
- Empty weight: 18,400 kg[13] (40,550 lb)
- Loaded weight: 25,300 kg (56,660 lb)
- Max takeoff weight: 34,500 kg (76,060 lb)
- Powerplant: 2× Saturn 117S/AL-41F1A turbofans
- Maximum speed: Mach 2.25 (2,390 km/h, 1,500 mph) at altitude
- Range: 3,600 km (1,940 nmi) ; (1,580 km, 850 nmi near ground level)
- Ferry range: 4,500 km (2,430 nmi) with external fuel tanks
- Service ceiling: 18,000 m (59,100 ft)
- Rate of climb: >280 m/s (>55,100 ft/min)
- Wing loading: 408 kg/m² (84.9 lb/ft²)
- Thrust/weight: 1.14
- Irbis-E passive phased array radar
- Internal 30 mm GSh-301 gun with 150 rounds.
- 8000 kg, distribute on 12 pylons for a variety of ordinance including air-to-air missiles, air-to-surface missiles, rockets, and bombs
- AA-10 Alamo: R-27R, R-27ER, R-27T, R-27ET, R-27EP
- AA-12 Adder: R-77, and the proposed R-77M1, R-77T
- AA-11 Archer: R-73E, R-73M, R-74M
- AS-17 Krypton: Kh-31A, Kh-31P Anti-Radiation Missile
- AS-20: Kh-59
- AS-14 Kedge: Kh-29T, Kh-29L
- KAB-500 Laser-guided bomb
- KAB-1500 Laser-guided bomb
- LGB-250 laser-guided bomb
- FAB-250 250kg unguided bombs
- FAB-500 500kg unguided bombs
- S-25LD laser-guided rocket, S-250 unguided rocket
- B-8 unguided S-8 rocket pods
- B-13 unguided S-13 rocket pods
Sukhoi Su-30 (air-to-air and air-to-surface)
- Crew: 2
- Length: 21.935 m (72.97 ft)
- Wingspan: 14.7 m (48.2 ft)
- Height: 6.36 m (20.85 ft)
- Wing area: 62.0 m² (667 ft²)
- Empty weight: 17,700 kg (39,021 lb)
- Loaded weight: 24,900 kg (54,900 lb)
- Max takeoff weight: 34,500 kg (76,060 lb)
- Powerplant: 2× AL-31FL low-bypass turbofans
- Dry thrust: 7,600 kgf (74.5 kN, 16,750 lbf) each
- Thrust with afterburner: 12,500 kgf (122.58 kN, 27,560 lbf) each
- Maximum speed: Mach 2.0 (2,120 km/h, 1,320 mph)
- Range: 3,000 km (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: 401 kg/m² (82.3 lb/ft²)
- Thrust/weight: 1.0
The Su-27PU had 8 hardpoints for its weapon load, whereas the Su-30MK's combat load is mounted on 12 hardpoints: 2 wingtip AAM launch rails, 3 pylons under each wing, 1 pylon under each engine nacelle, and 2 pylons in tandem in the "arch" between the engines. All versions can carry up to 8 tonnes of external stores.
- Guns: 1 × GSh-30-1 gun (30 mm caliber, 150 rounds)
- AAMs: 6 × R-27ER1 (AA-10C), 2 × R-27ET1 (AA-10D), 6 × R-73E (AA-11), 6 × R-77 RVV-AE(AA-12)
- ASMs: 6 × Kh-31P/Kh-31A anti-radar missiles, 6 × Kh-29T/L laser guided missiles, 2 × Kh-59ME
- Aerial bombs: 6 × KAB 500KR, 3 × KAB-1500KR, 8 × FAB-500T, 28 × OFAB-250-270
MiG-35 (multi-purpose)
- Crew: one or two
- Length: 19 m (62 ft 4 in)
- Wingspan: 15 m (49 ft 3 in)
- Height: 6 m (19 ft 8 in)
- Empty weight: 11,000 kg (24,250 lb)
- Loaded weight: 17,500 kg (38,600 lb)
- Max takeoff weight: 29,700 kg (65,500 lb)
- Powerplant: 2× Klimov RD-33MK afterburning turbofans
- Dry thrust: 5,400 kgf, 53.0 kN (11,900 lbf) each
- Thrust with afterburner: 9,000 kgf, 88.3 kN (19,800 lbf) each
- Maximum speed: Mach 2.25 (2,400 km/h, 1,491 mph) at altitude
- Range: 2,000 km (1,240 mi)
- Ferry range: 3,100 km (1,930 mi) with 3 external fuel tanks
- Service ceiling: 17,500 m (57,400 ft)
- Rate of climb: 330 m/s (65,000 ft/min)
- Thrust/weight: 1.03
- Guns: 1× 30 mm GSh-30-1 cannon, 150 rounds
- Hardpoints: 9 total (8× under-wing, 1× centre-line) with a capacity of over 6,500 kg external fuel and ordnance[citation needed]
- Rockets: S-8, S-13, S-24, S-25L, S-250 unguided and laser-guided rockets
- Missiles:
- Air-to-air:
- AA-10 Alamo: 4× R-27R, R-27T, R-27ER, R-27ET
- AA-8 Aphid: 4× R-60M
- AA-11 Archer: 8× R-73E, R-73M, R-74M
- AA-12 Adder: 8× R-77
- Air-to-surface:
- AS-17 Krypton: 4× Kh-31A, Kh-31P
- AS-14 Kedge: 4× Kh-29T, Kh-29L
- AS-20: 4× Kh-59
- Air-to-air:
- Bombs:
- Guided:
- KAB-500L: 500 kg laser-guided bomb
- KAB-500T: 500 kg TV-guided bomb
- Unguided:
- FAB-250: 250 kg bomb
- FAB-500: 500 kg bomb
- ZAB-500 fuel-air explosive Bomb
- Guided:
- Phazotron Zhuk AE AESA radar (or other members of the Zhuk radar family) [23]
- NII PP Optical Locator System
B-52 (heavy Bomber)
- Crew: 5 (pilot, copilot, radar navigator (bombardier), navigator, and Electronic Warfare Officer)
- Length: 159 ft 4 in (48.5 m)
- Wingspan: 185 ft 0 in (56.4 m)
- Height: 40 ft 8 in (12.4 m)
- Wing area: 4,000 sq ft (370 m²)
- Airfoil: NACA 63A219.3 mod root, NACA 65A209.5 tip
- Empty weight: 185,000 lb (83,250 kg)
- Loaded weight: 265,000 lb (120,000 kg)
- Max takeoff weight: 488,000 lb (220,000 kg)
- Powerplant: 8× Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf (76 kN) each
- Fuel capacity: 47,975 U.S. gal (39,948 imp gal; 181,610 L)
- Zero-lift drag coefficient: 0.0119 (estimated)
- Drag area: 47.60 sq ft (4.42 m²)
- Aspect ratio: 8.56
- Maximum speed: 560 kt (650 mph, 1,000 km/h[6])
- Combat radius: 4,480 mi (3,890 NM, 7,210 km)
- Ferry range: 10,145 mi (8,764 nm, 16,232 km)
- Service ceiling: 50,000 ft[6] (15,000 m)
- Rate of climb: 6,270 ft/min.[125] (31.85 m/s)
- Wing loading: 120 lb/ft² (595 kg/m²)
- Thrust/weight: 0.31
- Lift-to-drag ratio: 21.5 (estimated)
- Guns: 1× 20 mm (0.787 in) M61 Vulcan cannon in a remote controlled tail turret, removed from all current operational aircraft
- Bombs: Approximately 70,000 pounds (31,500 kg) mixed ordnance -- bombs, mines, missiles, in various configurations[6]
- Electro-optical viewing system that uses platinum silicide forward-looking infrared and high resolution low-light-level television sensors[145]
- Sniper Advanced Targeting Pod[146]
TU- 160 (heavy bomber)
- Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
- Length: 54.1 m (177 ft 6 in)
- Wingspan:
- Spread (20° sweep): 55.70 m (189 ft 9 in)
- Swept (65° sweep): 35.60 m (116 ft 10 in)
- Height: 13.10 m (43 ft 0 in)
- Wing area:
- Spread: 400 m² (4,310 ft²)
- Swept: 360 m² (3,875 ft²)
- Empty weight: 110 t[23] (242,000 lb)
- Loaded weight: 267 tonnes[23] (590,000 lb)
- Max takeoff weight: 275 tonnes[23] (606,000 lb)
- Powerplant: 4× Kuznetsov NK-32[23] turbofans
- Dry thrust: 137 kN (30,900 lbf) each
- Thrust with afterburner: 245 kN (55,100 lbf) each
- Maximum speed: Mach 2.05[24] (2,220 km/h, 1,380 mph) at high altitude
- Range: 12,300 km[25] (7,643 mi) practical range without in-flight refuelling, Mach 0.77 and carrying 6 × Kh-55SM dropped at mid range and 5% fuel reserves[25]
- Combat radius: 7,300 km[23] (4,536 mi)
- Service ceiling: 16,000 m[23] (49,200 ft)
- Rate of climb: 70 m/s (13,860 ft/min)
- Wing loading: 743 kg/m² with wings fully swept (152 lb/ft²)
- lift-to-drag: 18.5-19, while supersonic it is above 6.[26]
- Thrust/weight: 0.37
- 2 internal bays for 40,000 kg (88,185 lb) of ordnance, options include:
- 2 internal rotary launchers each holding 6 × Raduga Kh-55 cruise missiles (primary armament) or 12× Raduga Kh-15 short-range nuclear missiles
ll- 78 (Air refueling Tanker)
- Crew: Six
- Capacity: 138,000 kg (304,233 lb) of fuel
- Length: 46.59 m (152 ft 10 in)
- Wingspan: 50.50 m (165 ft 8 in)
- Height: 14.76 m (37 ft 1 in)
- Wing area: 300 m² (3,230 ft²)
- Empty weight: 72,000 kg (202,821 lb)
- Useful load: 85,720 kg (188,980 lb)
- Max takeoff weight: 210,000 kg (462,962 lb)
- Powerplant: 4× Aviadvigatel D-30 KP turbofan engines, 118 kN (26,500 lbf) each
- Special equipment: 3 x UPAZ-1M 'Sakhalin', (standardized suspended refueling unit), refueling pods; Two on pylons under the outer wings, and the third on the port side of the rear fuselage.
- Maximum speed: 850 km/h (460 kn, 530 mph)
- Range: 7,300 km (3,942 nmi, 4,551 mi)
- Service ceiling: 12,000 m (39,360 ft)
- Thrust/weight: 0.23
Mi- 24 (Gunship)
- Crew: 2-3: pilot, weapons system officer and technician (optional)
- Capacity: 8 troops or 4 stretchers
- Length: 17.5 m (57 ft 4 in)
- Rotor diameter: 17.3 m (56 ft 7 in)
- Wingspan: 6.5 m (21 ft 3 in)
- Height: 6.5 m (21 ft 3 in)
- Disc area: 235 m² (2,530 ft²)
- Empty weight: 8,500 kg (18,740 lb)
- Max takeoff weight: 12,000 kg (26,500 lb)
- Powerplant: 2× Isotov TV3-117 turbines, 1,600 kW (2,200 hp) each
- Maximum speed: 335 km/h (208 mph)
- Range: 450 km (280 miles)
- Service ceiling: 4,500 m (14,750 ft)
- flexible 12.7 mm Yakushev-Borzov Yak-B Gatling gun on most variants. Maximum of 1,470 rounds of ammunition.
- fixed twin-barrel GSh-30K on the Mi-24P. 750 rounds of ammunition.
- flexible twin-barrel GSh-23L on the Mi-24VP and Mi-24VM. 450 rounds of ammunition.
- PKT passenger compartment window mounted machine guns
- Total payload is 1,500 kg of external stores.
- Inner hardpoints can carry at least 500 kg
- Outer hardpoints can carry up to 250 kg
- Wing-tip pylons can only carry the 9M17 Phalanga (in the Mi-24A-D) or the 9K114 Shturm complex (in the Mi-24V-F).
- Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), Up to 500 kg.
- MBD multiple ejector racks (presumably MBD-4 with 4xFAB-100)
- KGMU2V submunition/mine dispenser pods
Eurocopter Tiger (attack Helicopter)
- Crew: 2 (pilot, weapon systems officer)
- Length: 14.08 m fuselage (46 ft 2 in)
- Rotor Diameter 13.00 m (42 ft 8 in)
- Height: 3.83 m (12 ft 7 in)
- Disc Area: 133 m² (1,430 ft²)
- Empty Weight: 3,060 kg (6,750 lb)
- Max Takeoff Weight: 6,000 kg (13,000 lb)
- Internal Fuel Capacity: 1,080 kg (2,380 lb)
- Powerplant: 2×Rolls-Royce/Turbomeca/MTU MTR390 turboshafts, 873 kW (1,170 shp)
Max Speed290 km/h with mast, 315 km/h without mast (157 knots, 181 mph with mast, 170 knots or 196 mph without mast)
Range:800 km (430 nm, 500 mi) combat (with external tanks in the inboard stations: 1300km)
Service Ceiling: 4,000 m (13,000 ft)
Rate of Climb10.7 m/s (2,105 ft/min)
Guns: 1× 30 mm (1.18 in) GIAT 30 cannon in chin turret On its two inner hardpoints and two outer hardpoints the Eurocopter Tiger can carry a combination of the following weapons:
- on each of its two inner hardpoints:
- 2x 20 mm (0.787 in) machine cannons in a pod, or
- 22× 68 mm (2.68 in) SNEB unguided missiles in a pod, or
- 8x AGM-114 Hellfire laser guided missiles
- on each of its two outer hardpoints:
- 2× Mistral air-to-air missiles, or
- 12× 68 mm (2.68 in) SNEB unguided missiles in a pod
Armor: 80% carbon fiber reinforced polymer and kevlar, 11% aluminium, and 6% titanium; capable of stopping 23 mm autocannon fire
Installed in the helicopter are a AN/AAR-60 MILDS System ensuring radar warning, a laser warning system, and a missile launch/approach detector developed by EADS DE, all connected to a central processing unit from Thales and a SAPHIR-M chaff/flare dispenser from MBDA. Its visual, radar, infrared, sound signatures have been minimized
Ka- 52 (Attack Helicopter)
- Crew: One (for Ka-52: two)
- Length: 13.50 m (44 ft 3 in)
- Rotor diameter: 2x 14.50 m (2x 47 ft 7 in)
- Height: 5.4 m (17 ft 9 in)
- Disc area: 330.3 m² (3,555 ft²)
- Empty weight: 7,800 kg (17,200 lb)
- Loaded weight: 9,800 kg (21,600 lb)
- Max takeoff weight: 10,800 kg (23,810 lb)
- Powerplant: 2× Klimov TV3-117VK turboshafts, 1,660 kW (2,226 shp) each
- For Ka-52:
- Loaded weight: 10,400 kg (22,930 lb)
- Maximum speed: 390 km/h (204 knots, 242 mph) in dive
- Cruise speed: 270 km/h (146 knots, 168 mph)
- Range: 1,160 km (720 miles)
- Combat radius: 460 km (286 miles)
- Service ceiling: 5,500 m (18,000 ft)
- Rate of climb: 16 m/s (52.5 ft/s)
- Disc loading: 30 kg/m² (6 lb/ft²)
- Power/mass: 0.33 kW/kg (0.20 hp/lb)
- 1x mobile semi-rigid 30 mm Shipunov 2A42 cannon (240 rounds, dual feeding AP or HE-Frag)
- A variety of payloads on the four under-wing hardpoints, including 23 mm UPK-23-250 gun pods (240 rounds each), APU-6 9K121 Vikhr anti-tank missile racks, Vympel R-73 (NATO: AA-11 Archer) air-to-air missiles, 80 mm S-8 rocket and 122 mm S-13 rocket pods, Kh-25 semi-active laser guided tactical air-to-ground missiles, presumably S-25/S-25L high caliber rockets, 4x 250 kg (550 lb) bombs or 2x 500 kg (1,100 lb) bombs, 500 L (130 US gal) external fuel tanks. Reportedly, twin Igla light air-to-air missile launchers under each wingtip countermeasure pod (total 4 missiles). Maximum total payload 2,000 kg.
- Two pods on the wingtips with flare and chaff countermeasure dispensers, 64 cartridges each (total 128).
Mi- 28 (Attack Helicopter)
- Crew: 1 pilot (rear), 1 navigator/weapons operator (front)
- Length: 17.01 m (55 ft 9 in)
- Rotor diameter: 17.20 m (56 ft 5 in)
- Height: 3.82 m (12 ft 7 in)
- Empty weight: 8,095 kg (17,845 lb)
- Loaded weight: 10,400 kg (22,930 lb)
- Max takeoff weight: 11,500 kg (25,705 lb)
- Powerplant: 2× Klimov TV3-117VMA turboshaft, 1,450 kW (1,950 hp) each
- Maximum speed: 302 km/h (187 mph)
- Range: 1,100 km (640 mi)
- Service ceiling: 5,800 m (19,000 ft)
- 1x chin-mounted 30 mm Shipunov 2A42 cannon with 300 rounds (220° horizontal fire)
- up to 2,300 kg of disposable stores on four hardpoints, including bombs, rockets, missiles, and gunpods
- Crew: two, pilot and weapons operator
- Length: 17.01 m (55 ft 10 in)
- Main rotor diameter: 17.20 m (56 ft 5 in)
- Height: 3.82 m (12 ft 6 in) (without radar)
- Main rotor area: 232.4 m² (2,500 ft²)
- Empty: 7,890 kg (17,394 lb)
- Loaded: 10,400 kg (22,930 lb)
- Maximum takeoff: 12,100 kg (26,700 lb)
- Powerplant: 2x Klimov TV3-117VM turboshafts, 1,640 kW (2,200 shp) each
- Maximum speed: 377 km/h (218 mph)
- Range: 460 km (286 miles)
- Service ceiling: 5,750 m (18,900 ft)
- Rate of climb: 816 m/min (2,680 ft/min)
- Main rotor loading: 45 kg/m² (9 lb/ft²)
- Power/Mass: 0.31 kW/kg (0.19 hp/lb)
- 1x chin-mounted 30 mm Shipunov 2A42 cannon with 300 rounds (220° horizontal fire)
- up to 2,400 kg (4,400 lb) of disposable stores on four hardpoints including bombs, rockets, gunpods, anti-tank and anti-air missiles.
Mi- 26 (heavy Transport)
- Crew: Six – 2 pilots, 1 navigator, 1 flight engineer, 1 loadmaster, 1 radio/electronic systems operator
- Capacity:
- Length: 40.025 m (131 ft 4 in) (rotors turning)
- Rotor diameter: 32.00 m (104 ft 11.8 in)
- Height: 8.145 m (26 ft 9 in)
- Disc area: 789 m2 (8,495 ft²)
- Empty weight: 28,200 kg (62,170 lb)
- Loaded weight: 49,500 kg (108,900 lb)
- Max takeoff weight: 56,000 kg (123,500 lb)
- Powerplant: 2× Lotarev D-136 turboshafts, 8,380 kW (11,240 shp) each
- Maximum speed: 295 km/h, 183 mph (160 kt)
- Range: 1,952 km, 1,240 miles (1,080 nautical miles)
- Service ceiling: 4,600 m (15,100 ft)
Ka- 60 (light transport)
- Crew: Two
- Capacity: Up to 16 infantry troops or 6 stretchers
- Length: 15.60 m (51 ft 2 in)
- Rotor diameter: 13.50 m (44 ft 3 in)
- Height: 4.20 m (13 ft 9 in)
- Loaded weight: 6,750 kg (14,850 lb)
- Useful load: 2,750 kg (external) (6,050 lb)
- Max takeoff weight: 6,750 kg (14,850 lb)
- Powerplant: 2× Rybinsk RD-600V turboshafts, 956 kW (1,282 shp) each
- * Fuselage width : 2.50 m (8 ft 2 in)
- Tail rotor diameter: 1.2 m (4 ft 6 in)
- Maximum speed: 300 km/h (162 knots, 185 mph)
- Cruise speed: 270 km/h (145 knots, 166 mph)
- Range: 615 km (332 NM, 380 mi)
- Service ceiling: 5,100 m (16,730 ft)
- Rate of climb: 10.4 m/s (2,047 ft/min) at sea level