Tuesday, 31 January 2012

A-10 Thunderbolt II

A-10 Thunderbolt II
 A-10 Thunderbolt II
 A-10 Thunderbolt II
 A-10 Thunderbolt II 
A-10 Thunderbolt II Dropping Bomb

Sunday, 22 January 2012

Sukhoi Su-27

Sukhoi Su-27
 Sukhoi Su-27 Flanker Air Brakes
 Sukhoi Su-27 Flanker Climbing

 Sukhoi Su-27 Flanker Shooting Flares
 Sukhoi Su-27

Sukhoi Su-27 Inverted

Sukhoi Su-27

Sukhoi Su-27
 Sukhoi Su-27 Flares
Su-27 Formation
 Sukhoi Su-27 Fleet
 Sukhoi Su-27 Flanker
 Sukhoi Su-27 Flanker Taking Off
Sukhoi Su-27

Sukhoi Su-27

Sukhoi Su-27
 Sukhoi Su-27 Fleet
 Sukhoi Su-27 Climbing
Su-27 Taking Off
 Sukhoi Su-27
Sukhoi Su-27 Formation

Sukhoi Su-27

Sukhoi Su-27
 The Sukhoi Su-27 (Flanker) is powered by twin-engine single seat 
 supermanoeuverable fighter aircraft designed by Sukhoi.Su-27 can be 
compared from the United States fourth generation fighters.Su-27 is 
able to perform almost all combat operations.There are several variants of
Su-27 such as Sukhoi Su-30,Sukhoi Su-33,Sukhoi Su-34,Sukhoi Su-35,Sukhoi
,Su-37,Shenyang J-11.
General characteristics/ specifications
Crew: 1
Length: 21.9 m (72 ft)
Wingspan: 14.7 m (48 ft 3 in)
Height: 5.92 m (19 ft 6 in)
Wing area: 62 m² (667 ft²)
Empty weight: 16,380 kg (36,100 lb)
Loaded weight: 23,430 kg (51,650 lb)
Max. takeoff weight: 30,450 kg (67,100 lb)
Powerplant: 2 × Saturn/Lyulka AL-31F turbofans
Dry thrust: 7,670 kgf (75.22 kN, 16,910 lbf) each
Thrust with afterburner: 12,500 kgf (122.6 kN, 27,560 lbf) each
Leading edge sweep: 42°

Maximum speed: Mach 2.35 (2,500 km/h, 1,550 mph) at altitude
Range: 3,530 km (2,070 mi) at altitude; (1,340 km / 800 mi at sea level)
Service ceiling: 18,500 m (62,523 ft)
Rate of climb: 300 m/s (54,000 ft/min)
Wing loading: 371 kg/m² (76 lb/ft²)
Thrust/weight: 1.07

1 × 30 mm GSh-30-1 cannon with 150 rounds
8,000 kg (17,600 lb) on 10 external pylons
Up to 6 × medium-range AA missiles R-27, 2 × short-range heat-seeking AA missiles R-73
Su-27S armament
30 mm GSH-30 Cannon, 150 rounds
6 × Medium-Range R-27R, R-27ER, R-27T, R-27ET
4 × Short-Range R-73E
Su-27SM armament
6 x Vympel R-77 advanced medium-range missile
4 x KAB-500KR and KAB-500L Guided Bombs
4 x Kh-29
4 x Kh-31
10 x Kh-35

Bell Boeing V-22 Osprey

Bell Boeing V-22 Osprey
CV-22 Osprey
 Bell Boeing V-22 Osprey
 Bell Boeing V-22 Osprey 
 Bell Boeing V-22 Osprey in dust

 Bell Boeing V-22 Osprey on Aircraft carrier
 V-22 Osprey on Rescue mission
V-22 Osprey Dropping Troops

Bell Boeing V-22 Osprey

Bell Boeing V-22 Osprey
 Bell Boeing V-22 Osprey
C V-22 Osprey
 V-22 Osprey Hovering
 Bell Boeing V-22 Osprey Gun ship
 V-22 Osprey
Bell Boeing V-22 Osprey

Bell Boeing V-22 Osprey

Bell Boeing V-22 Osprey

The V-22 Osprey is a tiltrotor aircraft that combines the
vertical takeoff, hover and vertical landing qualities of a
helicopter with the long-range, fuel efficiency and
speed characteristics of a turboprop aircraft.
Its mission is to conduct long-range infiltration, exfiltration
and resupply missions for special operations forces.

General characteristics / Specifications

Crew: Four (pilot, copilot and two flight engineers/crew cheifs)
24 troops (seated), 32 troops (floor loaded), or
20,000 lb (9,070 kg) of internal cargo, or up to 15,000 lb (6,800 kg) of external cargo (dual hook)
1× Growler light internally transportable ground vehicle
Length: 57 ft 4 in (17.5 m)
Rotor diameter: 38 ft 0 in (11.6 m)
Wingspan: 45 ft 10 in (14 m)
Width with rotors: 84 ft 7 in (25.8 m)
Height: 22 ft 1 in/6.73 m; overall with nacelles vertical (17 ft 11 in/5.5 m; at top of tailfins)
Disc area: 2,268 ft² (212 m²)
Wing area: 301.4 ft² (28 m²)
Empty weight: 33,140 lb (15,032 kg)
Loaded weight: 47,500 lb (21,500 kg)
Max. takeoff weight: 60,500 lb (27,400 kg)
Powerplant: 2 × Rolls-Royce Allison T406/AE 1107C-Liberty turboshafts, 6,150 hp (4,590 kW) each

Maximum speed: 275 knots (509 km/h, 316 mph) at sea level / 305 kn (565 km/h; 351 mph) at 15,000 ft (4,600 m)
Cruise speed: 241 knots (277 mph, 446 km/h) at sea level
Range: 879 nmi (1,011 mi, 1,627 km)
Combat radius: 390 nmi (426 mi, 722 km)
Ferry range: 1,940 nmi (2,230 mi, 3,590 km) with auxiliary internal fuel tanks
Service ceiling: 25,000 ft (7,620 m)
Rate of climb: 2,320 ft/min (11.8 m/s)
Disc loading: 20.9 lb/ft² at 47,500 lb GW (102.23 kg/m²)
Power/mass: 0.259 hp/lb (427 W/kg)

1× 7.62 mm (0.308 in) M240 machine gun or 0.50 in (12.7 mm) M2 Browning machine gun on ramp, removable
1× 7.62 mm (.308 in) GAU-17 minigun, belly-mounted, retractable, video remote control in the Remote Guardian System

V-22 Osprey in Night

CV-22 Osprey

Saturday, 14 January 2012

Chengdu J-10

Chengdu J-10

 Chengdu J-10 Aerobatics
 Chengdu J-10 Air Brakes
Chengdu J-10 Climbing