The newest addition to Pacific Aviation Museum’s collection is a Navy SH-60B Seahawk helicopter. The Sikorsky Seahawk is a navalized version of the Army’s UH-60 Blackhawk. The Army began using the Blackhawk in 1979. The Navy quickly saw the Blackhawk as a good foundation for replacing its SH-2 Sea Sprite, which was protecting individual ships such as frigates, destroyers, and cruisers, which often have to operate outside of the fleet’s protection umbrella. In effect, the Sea Sprite was a self-contained antisubmarine warfare (ASW) system. The 1960s-vintage Sea Sprite was too small and underpowered to support the Navy’s new LAMPS II avionics system. The Blackhawk was the ideal size for the new system, and most of its development cost had already occurred. The Navy called its Sea Sprite replacement the SH-60B, where the “S” stands for antisubmarine warfare. The Navy began using the Seahawk in 1984.

Although the AH-6B Seahawk is primarily an antisubmarine warfare aircraft, it has secondary capabilities for rescue and anti-surface warfare. Like all naval versions, it has a personnel winch for rescue purposes. In addition, all Blackhawk derivatives are highly modular, and the Seahawk’s torpedoes can be replaced by hellfire guided missiles, and it can carry machine guns or even a 30 mm cannon (although the cannon is primarily for clearing minefields).

The Navy was very happy with the Seahawk, so it ordered versions to replace many of its other helicopters. For central fleet protection, the Navy used the big Vietnam War-era SH-3 Sea King. The Navy replaced the Sea King with the SH-60F Seahawk. For Marine troop assault, the MH-60S Seahawk replaced the Vietnam-era CH-46 Sea Knight assault helicopter. The “M” stands for “multimission.”

An ASW helicopter needs to find enemy submarines lurking near the fleet. One way to do this is to deploy a long wire behind the helicopter. This magnetic anomaly detector, or MAD, can detect the presence of submarines at considerable depth. The SH-60B has its MAD boom on the right rear of the aircraft.

The SH-60B also has sonobuoys that it can drop in the water to listen for submarine and report its findings to the aircraft. Instead of having a left-side door, the SH-60 has a large window for the operator and 25 sonobuoy tubes. The aircraft can drop sonobuoys over a considerable area to provide a ring of protection around the fleet. It also has modular sensors in its nose that can be adapted to particular missions.

What if the aircraft finds an enemy submarine? The SH-60B can carry one Mk 46, Mk 50, or Mk 54 torpedo on each side. These torpedoes actively seek underwater targets after they are dropped.

The Blackhawk/Seahawk family of helicopters (and the Air Force’s PAVE Hawk and the Coast Guard’s Jay Hawk) grew out of experiences with the Vietnam era UH-1 Huey. Although the Huey had done an excellent job, its casualty rates were enormous. Bullets could easily damage critical systems, and if the helicopter crashed, the landing was likely to kill everyone in the aircraft. In terms of performance, the Huey had a very limited ability to carry passengers, internal cargo, and slung loads. This was particularly true in hot and high areas, such as the Vietnam highlands.

In the Blackhawk and its derivitives, critical systems are more “ballistic-resistant,” and the wheels fold in ways that can absorb a great deal of crash impact. In addition, seats are strong so that they do not collapse in a hard landing.

One requirement for the original Blackhawk design was that the aircraft has to be able to fit into a C-130 cargo hold. This resulted in an aircraft that is not very tall yet that is rather long. While the Huey cabin was a box, the UH-60 cabin is long and low. Navy versions have kept the same silhouette.

Table 1: Size and Performance Comparisons


UH-1D UH-60A SH-60B
Primary Mission Utility Utility ASW
Year Introduced 1959 1979 1984
Crew 2 pilots, 1 crew chiefs/gunner, 1 gunner 2 pilots, 2 crew chiefs/gunners 2 pilots, 1 or 2 weapons operators
Passengers 5-8 troops 14 troops


Length 57’ 1” (17.4 m) 64’ 10” (19.76 m) 64’ 8” (19.75m)
Rotor diameter 48’ 0” (14.63 m) 53’ 8” (16.36 m) 53’ 8” (16.35 m)
Height 14’ 5” (4.39 m) 16’ 10” (5.13 m) 17’ 2” (5.2 m)
Width 8’ 7” (2.62 m) 7’ 9” (2.36 m)
Empty Weight 5,215 lb (2,365 kg) 10,624 lb (4,819 m) 15,200 lb (6,895 kg)
Loaded/Gross Weight 9,049 lb (4,309 kg) 22,000 lb (9,980 kg) 17,758 lb (8,055 kg) ASW
Max Takeoff Weight 9,500 lb (4,309 kg) 23,500 lb (10,660 kg) 21,884 lb (9,927 kg)
Engine 1 x Lycoming T-53-L-11 2 x General Electric
2 x General Electric
Take-Off Power 1,100 shp (820 kW) 2 x 1,890 shp
(1,410 kW)
2 x 1,890 shp
(1,410 kW)
Maximum speed 135 mph
(117 kn, 217 km/h)
183 mph
(159 kn, 278 km/h)
207 mph
(180 kn, 333 km/h)
Cruise speed 173 mph
(150 kn, 278 km/h)
168 mph
(146 kn, 270 km/h)
Range 315 mi
(274 nmi, 507 km)
368 mi
(320 nmi, 592 km)
518 mi
(450 nmi, 834 km)

Source: Wikipedia, which has a good summary from other good sources. However, the UH-1D passenger capacity was reduced to reflect experience in Vietnam.

Post by Ray Panko


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