منتديات البسالة

الصفحات: 1 2 3

::::موسوعه الطائرات الحربية:::

اولا لان الموقع الى بجيب منه المعلومات انجليزى لازم تعرف بعض المصطلحات
primary function:المهمة الاساسية
contractor: المصنع
crew الفريق بتاع الطيارة
power plant:المحركات بتاعتها
length&heigh(معروفين)
wingspan:طول الجناح
weight:الوزن
speed :السرعه
range: المدى الى بتوصله
first flight:اول طلعه ليها
end of service:نهايت خدمة الطائرة
nuber built: عدد الطيارات من نوعها صنع؟؟

__________________

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]

A-5 Vigilante

Primary Function: Tactical reconnaissance, carrier-based attack aircraft
Contractor: North American / Rockwell
Crew: Two (pilot, navigator)
Unit Cost: N/A
Powerplant
Two turbojet General Electric J79-GE-8 engines (10,800 lb each)
Dimensions
Length: 76 ft 6 in (23.32 m)
Wingspan: 53 ft (16.15 m)
Height: 19 ft (5.79 m)
Weights
Empty: 37,500 lb (17,009 kg)
Maximum Takeoff: 79,588 lb (36,094 kg)
Performance
Speed: 1,385 mph (2,230 km/h)
Ceiling: 48,400 ft (14,752 m)
Range: 1,500 miles (2,415 km)
Armament
1 nuclear weapon, and conventional weapons on two hard points
Service Life
First Flight: August 31, 1958 (prototype)
1960 (A3J-1)
April 1962 (A-5B)
End of Service: November 20, 1979
Number Built: [156 total] [/align]

A-6 Intruder

Primary Function: All-weather medium attack aircraft
Contractor: Grumman
Crew: Two
Unit Cost: $22 million
Powerplant
Two Pratt & Whitney J52-P8B engines (9,300 pounds thrust each)
Dimensions
Length: 54 feet 7 inches (16.1 meters)
Wingspan: 53 feet (16.1 meters)
Height: 15 feet 7 inches (4.74 meters)
Weights
Empty: 25,630 pounds (11,636 kg)
Maximum Takeoff: 60,626 pounds (27,524 kg)
Performance
Speed: 563 knots (648 mph / 1036 km/h)
Ceiling: 40,600 feet
Range: 1,077 miles (1,733 km) -- full combat load
Armament
10 2.75" Rocket Pod
10 5" Zuni Rocket Pod
28 Mk-20 Rockeye
Mk-77 Napalm
28 Mk-81 (250 lbs)
28 Mk-82 Snakeye
13 Mk-83 (1,000 lbs)
5 Mk-84 (2,000 lbs)
20 Mk-117 (750 lbs)
28 CBU-78
GBU-10E Laser Guided Bomb
GBU-12D Laser Guided Bomb
GBU-16B Laser Guided Bomb
AGM-123A Skipper II
AGM-45 Shrike
AGM-62 Walleyes
AIM-9 Sidewinders

System Weapon Improvement Program, SWIP
AGM-88 HARMs
AGM-84E SLAMs
AGM-65 Maverick Anti-Ship Missile
AIM-120A AMRAAM
Service Life
First Flight: April 19, 1960 (A-6A)
February 27, 1970 (A-6E)
1963 (EA-6A)
May 25, 1968 (EA-6B)
End of Service: December 19, 1996
Number Built: A-6A (482) + 154 others [~636 total]

A-7 Corsair II Specifications

Primary Function: Attack
Contractor: Ling-Temco-Vought (Prime, now Northrop Grumman Corp.)
Crew: One
Unit Cost: $2,860,000 (A-7D)
Powerplant
Single Allison/Rolls Royce TF41-A-400 non-afterburning turbofan engine with a static thrust rating of 15,000 pounds
Dimensions
Length: 46 feet 1.5 inches
Wingspan: 38 feet 9 inches
Height: 16 feet 1 inch
Weights
Empty: 19,111 lb (8668 kg)
Maximum Takeoff: 42,000 lb (19050 kg)
Performance
Speed: 595 knots (685 mph / 1102 km/h)
Ceiling: 45,000 ft
Range: 3,224 miles
Armament
One internally mounted M61A1 20 mm six barrel cannon
Six wing pylons
Two fuselage launch stations
Pylons can carry a large single weapon, multiple racks capable of six weapons per rack, or triple racks with three weapons per rack.
Can carry 15,000 pounds of payload
Compatible with practically all first line ordnance used by the U.S./USAF/NATO.

Service Life
First Flight: September 27, 1965 (A-7A)
End of Service: 1993 (still in service with Greece and Portugal)
Number Built: A-7A (199) + A-7B (196) + A-7C (67) + 1,107 others [~1,569 total]

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 to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including 500 pounds (225 kilograms) of Mk-82 and 2,000 pounds (900 kilograms) of Mk-84 series low/high drag bombs, incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-inch (6.99 centimeters) rockets; illumination flares and AIM-9 Sidewinder missiles.
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.

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 conventional 500-pound bombs, or 30 CBU-87/89/97, or ZX JDAMS. Also can be reconfigured 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]

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