Specifications | |
Type | Shipboard ASW and anti-ship helicopter |
Program Summary | Latest in the H-2 series LAMPS MARK I program Entered the Fleet in 1967 and has operated from most aviation-capable ships in the U.S. Navy and international navies. Currently operated by the U.S. Naval Reserve Force; first delivered in February 1993. In 1995, the Arab Republic of Egypt contracted for 10 SH-2G aircraft in a dipping sonar configuration. The first deliveries under this program took place in 1997. The aircraft's low gross weight coupled with the power available from the T700-GE-401 engines make it attractive for small deck operations. |
Manufacturer | Kaman Aerospace Old Windsor Road Bloomfield, Connecticut 06002 |
Crew | three (2 pilots + 1 aircrew) |
Passengers | up to 8 fully armed troops |
Weapons | On outriggers on the fuselage side, the SH-2G can carry 2 x Mk.46 ASW torpedo 2 x Mk.50 ALWT torpedo Mk.11 depth charge 2 x Penguin anti-ship missile 2 x Maverick 2 x Sea Skua anti-ship missile Hellfire missiles 2.75 inch rockets |
Power plant | 2 x General Electric T700-GE-401 turboshafts |
Power | 2 x 1285 kW (1723 shp) contingency rating; 2 x 1690 shp for 30 minutes maximum 2 x 1437 shp maximum continuous. |
Fuel consumption | 0.21 kg/h/shp at intermediate power |
Fuselage length | 44ft (13.5m) |
Width | 12'4"ft (3.73m) |
Height | 15ft (4.62m) over tail rotor |
Main Rotor Diameter | 44ft 4in (13.5m) |
Tail rotor diameter | 8ft (2.46m) |
Empty Weight | 7,600lb (3,447kg) |
Max Loaded Weight | 13,500lb(6,124kg) |
Fuel | 1800 l /476 US gal) |
Useful load | 2300 kg |
Cargo hook capacity | 1810 kg |
Max. take-off weigth | 6115 kg |
Max. level speed | 159mph (256km/h) at sea level |
Normal cruise speed | 222 km/h (120 kts) |
Max. climb rate | 2,070 feet/min with Two Auxiliary Fuel Tanks (at sea level) 1,305 feet/min with One Engine (at sea level) |
Service ceiling | 20400 ft (6218m) |
Hover in ground effect | 17600 ft (5365m) |
Hover out of ground effect | 14600 ft (4450m) |
Max. range | 450 nautical miles (with 2 auxiliary fuel tanks) 1000 km (540 NM) at 5000 ft also cited |
Max. Endurance | 4.5 hours at 5000 feet 5.3 hrs at 5000 ft also cited |
Costs | In 1993 the SH-2F to SH-2G conversion was quoted as $12 million. Ten for Egypt cost $150 million |
Customers | US Navy - 6 new (plus rebuilds from SH-2Fs) Egypt - 10 (rebuilds) Australia - 11 (rebuilds) New Zealand - 4 (rebuilds) |
歡迎光臨 鐵之狂傲 (https://gamez.com.tw/) |