A-7 Corsair II
군사대국 | 2004-04-26 20:38:14
조회 2930 | 추천 2 | 다운로드 80
* Specifications *
Contractor: Ling-Temco-Vought (Prime, now Northrop Grumman Corp.)
Power Plant: Single Allison/Rolls Royce TF41-A-400 non-afterburning turbofan engine with a static thrust rating of 15,000 pounds
Accommodations: A-7E Pilot only
TA-7C Two seats
Performance (A-7E/TA/7C): Maximum speed at 20,000 feet Mach .94
Range greater than 1,900 nautical miles
External Dimensions:
Wing Span: 11.8m/ 38.73 ft
Wing span over missiles
Wing chord: at root 4.72m
Wing chord: at tip 1.18m
Wing aspect ratio: 4
Width, wings folded: 7.24m/ 23.77 ft
Aspect ratio: 4
Sweep 1/4 chord: 35°
Length overall: 14.06m/ 46.13 ft
Height overall: 4.90m/ 16.06 ft
MGC: 130.08 in
Tailplane span: 5.52m
Distance between fin tips: 17447
Wheel track: 2.90m
Maximum tread: 9.49 ft
Areas:
Wings, gross: 34.83m2/ 375 sq ft
Ailerons (total): 1.85m2
Leading-edge flaps (total): 3.46m2
Trailing-edge flaps (total): 4.04m2
Vert Tail Services (total)
Horz Tail Services (total)
Tailerons (total)
Weight (with TF41-A-2 engine):
Empty: 18,546 lbs / 8,676kg
Basic: 19,576 lbs
Design: 29,575 lbs
Combat (Clean A/P): 25,834 lbs
Maximum takeoff (Overload): 42,000 lbs
Maximum takeoff (Normal): 37,279 lbs
Maximum landing (Carrier): 25,300 lbs
Maximum fuel weight
Maximum external stores load
Performance (At Maximum Takeoff Weight of 19,050kg):
Max level speed @ S.L.: 600 knots
Max speed, intermediate power
Approach speed
T-O run @ maximum take-off weight: 1,705m
Contractor: Ling-Temco-Vought (Prime, now Northrop Grumman Corp.)
Power Plant: Single Allison/Rolls Royce TF41-A-400 non-afterburning turbofan engine with a static thrust rating of 15,000 pounds
Accommodations: A-7E Pilot only
TA-7C Two seats
Performance (A-7E/TA/7C): Maximum speed at 20,000 feet Mach .94
Range greater than 1,900 nautical miles
External Dimensions:
Wing Span: 11.8m/ 38.73 ft
Wing span over missiles
Wing chord: at root 4.72m
Wing chord: at tip 1.18m
Wing aspect ratio: 4
Width, wings folded: 7.24m/ 23.77 ft
Aspect ratio: 4
Sweep 1/4 chord: 35°
Length overall: 14.06m/ 46.13 ft
Height overall: 4.90m/ 16.06 ft
MGC: 130.08 in
Tailplane span: 5.52m
Distance between fin tips: 17447
Wheel track: 2.90m
Maximum tread: 9.49 ft
Areas:
Wings, gross: 34.83m2/ 375 sq ft
Ailerons (total): 1.85m2
Leading-edge flaps (total): 3.46m2
Trailing-edge flaps (total): 4.04m2
Vert Tail Services (total)
Horz Tail Services (total)
Tailerons (total)
Weight (with TF41-A-2 engine):
Empty: 18,546 lbs / 8,676kg
Basic: 19,576 lbs
Design: 29,575 lbs
Combat (Clean A/P): 25,834 lbs
Maximum takeoff (Overload): 42,000 lbs
Maximum takeoff (Normal): 37,279 lbs
Maximum landing (Carrier): 25,300 lbs
Maximum fuel weight
Maximum external stores load
Performance (At Maximum Takeoff Weight of 19,050kg):
Max level speed @ S.L.: 600 knots
Max speed, intermediate power
Approach speed
T-O run @ maximum take-off weight: 1,705m
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