HH-60A: Prototype for the HH-60D rescue helicopter. A modified UH-60A primarily designed for combat search and rescue. It is equipped with a rescue hoist with a 200 ft (60.96 m) cable that has a 600 lb (270 kg) lift capability, and a retractable in-flight refueling probe.
General characteristics
Crew: 4 (2 pilots, flight engineer, gunner)
Capacity: max. crew 6, 8–12 troops, plus litters and/or other cargo
Length: 64 ft 10 in (17.1 m)
Rotor diameter: 53 ft 8 in (14.1 m)
Height: 16 ft 8 in (5.1 m)
Empty weight: 16,000 lb (7,260 kg)
Max. takeoff weight: 22,000 lb (9,900 kg)
Powerplant: 2 × two General Electric T700-GE-700/701C free-turbine turboshafts, 1,630 shp (1,220 kW) each
Performance
Maximum speed: 195 knots (224 mph, 360 km/h)
Cruise speed: 159 kt (184 mph, 294 km/h)
Range: 373 mi (internal fuel), or 508 mi (with external tanks) (600 km, or 818 km)
Service ceiling: 14,000 ft (4,267 m)
Armament
2x 7.62 mm miniguns or
2x 0.50 in machine guns
Onboard Systems
INS/GPS/Doppler navigation
SATCOM satellite communications
Secure/anti-jam communications
LARS (Lightweight Airborne Recovery System) range/steering radio to compatible survivor radios
Automatic flight control
NVG night vision goggle lighting
FLIR forward looking infra-red radar
Color weather radar
Engine/rotor blade anti-ice system
Retractable In-flight refueling probe
Integral rescue hoist
RWR combat enhancement
IR infra-red jamming unit
flare/chaff countermeasure dispensing system