- Попробуйте сами сравнить: http://home.att.net/~jbaugher1/f111_9.html
Specification of the FB-111A:
Engines: Two Pratt & Whitney TF30-P-7 turbofans, 12,500 lb.s.t. dry and 20,350 lb.s.t. with afterburner. Performance: Maximum speed (clean): 1453 mph at 50,000 feet, 1320 mph at 36,000 feet, 838 mph at sea level. Initial climb rate (clean) 23,418 feet per minute. Service ceiling: 50,263 feet. Range: 2500 miles with four SRAMs and internal fuel only. Maximum ferry range: 4786 miles with six 600-US gall. auxiliary fuel tanks mounted on underwing pylons. Weights: 47,980 pounds empty, 119,250 pounds gross. Dimensions: Wingspan 70 feet 0 inches (minimum sweep), 33 feet 11 inches (maximum sweep), length 73 feet 6 inches, height 17 feet 0 inches. Internal fuel capacity of 5010 US gallons. With six 600 US gallon underwing drop tanks, a total of 9223 US gallons of fuel can be carried. Armed with up to six Boeing AGM-69A SRAMs on external pylons or in internal weapons bay, or a conventional ordnance load of up to 37,500 pounds of bombs, rockets, or fuel tanks. http://en.wikipedia.org/wiki/Su-34
General characteristics
Crew: Two
Length: 23.34 m (72 ft 2 in)
Wingspan: 14.7 m (48 ft 3 in)
Height: 6.09 m (19 ft 5 in)
Loaded weight: 39,000 kg (85,980 lb)
Max takeoff weight: 45,100 kg (99,425 lb)
Powerplant: 2× Lyulka AL-35F turbofans, 137.2 kN (30,845 lbf) with afterburner[citation needed] each
Performance
Maximum speed: Mach 1.6 at service ceiling (1,900 km/h, 1,200 mph) ; Mach 1.14 at sea level
Range: 4,000 km (2,800 mi) ferry range
Combat radius: 1,130 km (700 mi)
Service ceiling: 15,000 m (45,890 ft)
Wing loading: 629 kg/m² (129 lb/ft²)
Thrust/weight: 0.68
Armament
1× 30 mm GSh-30-1 (9A-4071K) cannon, 150 rounds
2× wingtip rails for R-73 (AA-11 'Archer') air-to-air missiles
10× wing and fuselage stations for up to 8,000 kg (17,630 lb) of ordnance, including Kh-29L/T, Kh-25MT/ML, Kh-25MP, Kh-36, Kh-38, Kh-41, Kh-59M, Kh-58, Kh-31P, Kh-35 Ural, Kh-41, Kh-65S, Kh-SD, 2 Moskit, 3 Jachont air-to-ground missiles, KAB-500L/KR or KAB-1500L guided bombs, unguided bombs, B-8 rocket pods with 20 80 mm S-8 rockets, B-13 rocket pods with 5 122 mm S-13 rockets, O-25 rocket pords with 1 340 mm S-25 rocket, fuel tanks, EW- and reconnaissance pods.
- Попробуйте сами сравнить: http://home.att.net/~jbaugher1/f111_9.html
Specification of the FB-111A:
Engines: Two Pratt & Whitney TF30-P-7 turbofans, 12,500 lb.s.t. dry and 20,350 lb.s.t. with afterburner. Performance: Maximum speed (clean): 1453 mph at 50,000 feet, 1320 mph at 36,000 feet, 838 mph at sea level. Initial climb rate (clean) 23,418 feet per minute. Service ceiling: 50,263 feet. Range: 2500 miles with four SRAMs and internal fuel only. Maximum ferry range: 4786 miles with six 600-US gall. auxiliary fuel tanks mounted on underwing pylons. Weights: 47,980 pounds empty, 119,250 pounds gross. Dimensions: Wingspan 70 feet 0 inches (minimum sweep), 33 feet 11 inches (maximum sweep), length 73 feet 6 inches, height 17 feet 0 inches. Internal fuel capacity of 5010 US gallons. With six 600 US gallon underwing drop tanks, a total of 9223 US gallons of fuel can be carried. Armed with up to six Boeing AGM-69A SRAMs on external pylons or in internal weapons bay, or a conventional ordnance load of up to 37,500 pounds of bombs, rockets, or fuel tanks. http://en.wikipedia.org/wiki/Su-34
General characteristics
Crew: Two
Length: 23.34 m (72 ft 2 in)
Wingspan: 14.7 m (48 ft 3 in)
Height: 6.09 m (19 ft 5 in)
Loaded weight: 39,000 kg (85,980 lb)
Max takeoff weight: 45,100 kg (99,425 lb)
Powerplant: 2× Lyulka AL-35F turbofans, 137.2 kN (30,845 lbf) with afterburner[citation needed] each
Performance
Maximum speed: Mach 1.6 at service ceiling (1,900 km/h, 1,200 mph) ; Mach 1.14 at sea level
Range: 4,000 km (2,800 mi) ferry range
Combat radius: 1,130 km (700 mi)
Service ceiling: 15,000 m (45,890 ft)
Wing loading: 629 kg/m² (129 lb/ft²)
Thrust/weight: 0.68
Armament
1× 30 mm GSh-30-1 (9A-4071K) cannon, 150 rounds
2× wingtip rails for R-73 (AA-11 'Archer') air-to-air missiles
10× wing and fuselage stations for up to 8,000 kg (17,630 lb) of ordnance, including Kh-29L/T, Kh-25MT/ML, Kh-25MP, Kh-36, Kh-38, Kh-41, Kh-59M, Kh-58, Kh-31P, Kh-35 Ural, Kh-41, Kh-65S, Kh-SD, 2 Moskit, 3 Jachont air-to-ground missiles, KAB-500L/KR or KAB-1500L guided bombs, unguided bombs, B-8 rocket pods with 20 80 mm S-8 rockets, B-13 rocket pods with 5 122 mm S-13 rockets, O-25 rocket pords with 1 340 mm S-25 rocket, fuel tanks, EW- and reconnaissance pods.
Спасибо, я люблю F-111 и Су-34, однако, как представляется, F-111 имеет радиус больше борьбы, чем Су-34 на внутренних топливных Однако с туалетом, так и Су-34 является более бомбардировщик
Я никогда не видел картину один Су-34 с топливными баками, может ли он нести топливных баков
Последний раз редактировалось МиГ-23; 31.12.2007 в 10:10.
Я бы сказал , что установка ПТБ на нем изначально не предусматривалась и этот вопрос в ТЗ не входил , а то слово "не способен " как-то ущербно звучит . Дальнейшие машины из семейства Су-27 ПТБ нести способны , Су-30/33/35.
Спасибо посмотрел ,а только нет там рвп ,есть такое выражение как "рвп молчит хороший знак значит куда надо ляжет гак"это из песни )рв -радиовысотомер ,а рвп что такое ?
Спасибо посмотрел ,а только нет там рвп ,есть такое выражение как "рвп молчит хороший знак значит куда надо ляжет гак"это из песни )рв -радиовысотомер ,а рвп что такое ?