موسوعه الطائرات الحربية ...

اولا لأن الموقع اللى بت منه المعلومات انجليزى لازم نتعرف على بعض المصطلحات
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primary function:المهمة الاساسية
contractor: المصنع
crew: فريق الطائره
power plant:المحركات
length&heigh(الطول والارتفاع)
wingspan:طول الجناح
weight:الوزن
speed :السرعه
range: المدى
first flight:اول طلعه للطائره
end of service:نهاية خدمة الطائرة
nuber built: عدد الطيارات من نوعها الذي تم صنعة؟؟

والان نحن جاهزين تمام وعلى جميع الاعضاء هنا في محطات عربية ربط احزمة مقاعدهم خوفا على سلامتهم

ههههههههههههههه

A-3 Skywarrior

Primary Function: Carrier-based nuclear bomber
Contractor: Douglas
Crew: Three (pilot, bombardier/navigator, ECM operator)
Unit Cost: N/A
Powerplant
Two Pratt & Whitney J57-P-10 turbojet engines rated at 10,500 lb thrust
Dimensions
Length: 76 ft. 4 in
Wingspan: 72 ft. 6 in
Height: 22 ft. 9.5 in
Weights
Empty: 39,409 lb
Maximum Takeoff: 70,000 lb
Performance
Speed: 610 mph
Ceiling: 41,000 ft
Range: 2,100 mi
Armament
Two 20mm cannons in rear, and up to 12,000 lb of weapons; option for nuclear weapons
Service Life
First Flight: March 1991 (XA3D-1 prototype)
September 16, 1953 (YA3D-1)
End of Service: March 1991
Number Built: [280 total]

A-4 Skyhawk

Primary Function: Attack/training aircraft
Contractor: McDonnell Douglas
Crew: One; two in trainer versions
Unit Cost: N/A
Powerplant
One P&W J-52-P-408A non-afterburning, turbojet engine rated at 11,220 lb thrust
Dimensions
Length: 41 ft, 8.5 in (including IFR probe)
Wingspan: 26 ft, 6 in
Height: 14 ft, 11.88 in
Weights
Empty: 10,250 lb
Max. Takeoff: 22,500 lb
Performance
Speed: 701 mph
Ceiling: 40,000 ft
Range: 720 miles (with max. ordnance)
Armament
Two Mk.12 20-mm cannons; bombs, rockets, ASMs, AIM-9 AAMs
Service Life
First Flight: June 22, 1954 (prototype)
August 14, 1954 (A-4A)
March 26, 1956 (A-4B)
August 21, 1958 (A-4C)
End of Service: N/A
Number Built: A-4A (166) + A-4B (542) + A-4C (638) + 1614 others [2,960 total]

يتبع
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AV-8B Harrier II

Primary Function: STOVL close-support
Contractor: McDonnell Douglas
Crew: One
Unit Cost: $23,700,000
Powerplant
one Rolls-Royce F402-RR-408 Pegasus (23,800 lb)
Dimensions
Length: 46.3 feet
Wingspan: 30.3 feet
Height: 11 feet, 7 inches
Weights
Empty: 14,867 lb
Maximum Takeoff: 31,000 lb
Performance
Speed: 1.0 Mach
Ceiling: 50,000+ feet
Combat Radius: 103 mi (90 nm / 167 km)
Armament
One fuselage-mounted 25 mm gun system
Standard Air-to-Ground (A/G) load: Six Mk 82, 500 pound bombs
Standard Air-to-Air (A/A) load: Four AIM-9L/M Sidewinder missiles
Provisions for carrying up to 9,000 pounds of ordnance on seven stations

Service Life
First Flight: November 9, 1978 (YAV-8B)
November 5, 1981 (AV-8B)
End of Service: N/A
Number Built: [340+ total]

A-10 Thunderbolt II (Warthog

Primary Function: close air support (A-10), airborne forward air control (OA-10)
Contractor: Fairchild Republic Co.
Crew: One
Unit Cost: $9.8 million (fiscal 98 constant dollars)
Powerplant
Two General Electric TF34-GE-100 turbofans (9,065 pounds each)
Dimensions
Length: 53 feet, 4 inches (16.16 meters)
Wingspan: 57 feet, 6 inches (17.42 meters)
Height: 14 feet, 8 inches (4.42 meters)
Weights
Empty: 25,600 lb
Maximum Takeoff: 51,000 lb (22950 kg)
Performance
Speed: 420 mph (Mach 0.56)
Ceiling: 45,000 feet (13636 meters)
Range: 800 miles (695 nm)
Armament
One 30 mm GAU-8/A seven-barrel Gatling gun; up to16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wingand three under-fuselage pylon stations, including 500 pounds (225kilograms) of Mk-82 and 2,000 pounds (900 kilograms) of Mk-84 serieslow/high drag bombs, incendiary cluster bombs, combined effectsmunitions, mine dispensing munitions, AGM-65 Maverick missiles andlaser-guided/electro-optically guided bombs; infrared countermeasureflares; electronic countermeasure chaff; jammer pods; 2.75-inch (6.99centimeters) rockets; illumination flares and AIM-9 Sidewindermissiles.
Service Life
First Flight: May 10, 1972 (prototype)
April 5, 1972 (A-10)
End of Service: N/A
Number Built: A-10A (721) + A-10B (30) [~751 total]

S-3 Viking

Primary Function: Antisubmarine Warfare, Sea Surveillance
Contractor: Lockheed
Crew: Four
Unit Cost: $27 million
Powerplant
Two General Electric TF-34-GE-400B turbofan engines rated at 9,275 lb thrust each
Dimensions
Length: 53 feet, 4 in
Wingspan: 68 feet, 8 in
Height: 22 feet, 9 in
Weights
Empty: 26,650 lb
Maximum Takeoff: 52,539 lb
Performance
Speed: 518 mph
Ceiling: 40,000 ft
Range: 2,645 mi
Armament
Up to 3,958 pounds of weapons, including AGM-84 Harpoon and AGM-65 Maverick missiles, torpedoes, mines, rockets and bombs.

يتبع ...
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[center]B-1b Lancer

Primary Function: Long-range, multi-role, heavy bomber
Contractor: Rockwell International, North American Aircraft
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Unit Cost: $283.1 million (fiscal 98 constant dollars)
Powerplant
Four General Electric F-101-GE-102 turbofan engines with afterburner (30,000-plus pounds with afterburner each)
Dimensions
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward /
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weights
Empty: 190,000 lb (86,183 kg)
Maximum Takeoff: 477,000 lb (216,634 kg)
Performance
Speed: 900-plus mph (Mach 1.2 at sea level)
Ceiling: 30,000+ feet (9,144+ meters)
Range: Intercontinental, unrefueled
Armament
Up to 84 Mark 82 conventional500-pound bombs, or 30 CBU-87/89/97, or ZX JDAMS. Also can bereconfigured to carry a wide range of nuclear weapons.
Service Life
First Flight: December 23, 1974 (B-1A)
October 18, 1984 (B-1B)
End of Service: N/A
Number Built: B-1A (4) + B-1B (100) [104 total]

B-2 Spirit

Primary Function: Multi-role heavy bomber
Contractor: Northrop Grumman Corp.
Crew: Two pilots
Unit Cost: Approximately $1.157 billion
Powerplant
Four General Electric F-118-GE-100 engines (17,300 lb each)
Dimensions
Length: 69 feet (20.9 meters)
Wingspan: 172 feet (52.12 meters)
Height: 17 feet (5.1 meters)
Weights
Empty: 162,000 lb (73,482 kg)
Typical Takeoff: 336,500 lb (152,634 kg)
Performance
Speed: High subsonic
Ceiling: 50,000 feet (15,152 meters)
Range: Intercontinental, unrefueled
Armament
NUCLEAR
16 B61
16 B83 CONVENTIONAL
80 MK82
16 MK84
36 CBU87
36 CBU89
36 CBU97 PRECISION
16 JDAM (2,000 lb GBU-31)
8 AGM-154 JSOW
8 GBU-37 Bunker Busters
8 EGBU-28 (Enhanced GBU-37)
AGM-158 (JASSM)

Service Life
First Flight: July 17, 1989 (B-2)
End of Service: N/A
Number Built: [21 total]

B-17 Flying Fortress

Primary Function: Heavy bomber
Contractor: Boeing
Crew: 10 (Pilot, Co-Pilot, Engineer, Bombardier, Radioman, 5 Gunners)
Unit Cost: $276,000 (B-17G)
Powerplant
Four 1,200 h.p. Wright R-1820-97 radial piston engines
Dimensions
Length: 74 feet, 4 inches (22.66 m)
Wingspan: 103 feet, 10 inches (31.65 m)
Height: 19 feet, 1 inch (5.82 m)
Weights
Empty: 36,135 lb
Maximum Takeoff: 54,000 lb (gross)
Performance
Speed: 300 mph (483 km/h)
Ceiling: 35,000 ft (10667 m)
Range: 1,850 miles (2979 km)
Armament
Thirteen .50 caliber machine guns, up to 17,600 lb.(short range) bombload
Service Life
First Flight: July 28, 1935 (prototype)
December 2, 1936 (Y1B-17A)
End of Service: May 1945
Number Built: [12,726 total]

F-106 Delta Dart

Primary Function: All-weather interceptor
Contractor: Convair
Crew: One
Unit Cost: $3,305,435
Powerplant
One Pratt & Whitney J75-P-17 of 24,500 pounds thrust with afterburner
Dimensions
Length: 70 feet, 9 inches
Wingspan: 38 feet, 4 inches (A model)
Height: 20 feet, 4 inches
Weights
Empty: N/A
Maximum Takeoff: N/A
Performance
Speed: 1,525 mph
Ceiling: 53,000 feet (A model)
Range: 1,500 miles (A model)
Armament
One AIR-2A Genie air to-air nuclear missile, Four AIM-4 Falcon air-to-air missiles, M61A1 Vulcan 20MM Cannon

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