Its capabilities include transport for 11 combat-ready air assault troops and a 105 mm howitzer with 30 rounds of ammunition.
It was first flown in October 1974 and was developed in part by the Utility Tactical Transport Aircraft System (UTTAS) program. Sikorsky and Boeing were the two competing companies selected to produce an aircraft to satisfy the requirements of the Army. Sikorsky ultimately won out in December of 1976.
Due to the high level of technology involved in producing a Black Hawk helicopter, when they are shot down or lost in combat, explosive charges that are found in the aircraft are detonated. This incinerates the helicopter to prevent the classified technology from falling into the hands of enemies.
The specifications of the Black Hawk helicopter are listed below:
Specifications:
Manufacturer | Sikorsky Aircraft |
Performance | Max Cruise Speed |
4,000 ft; 95°F 152 knots | |
2,000 ft; 70°F 159 knots | |
SLS 155 knots | |
VNE 193 knots | |
Vertical rate of Climb | 95% MRP |
4,000 ft; 95°F 1,550 ft per minute | |
2,000 ft; 70°F 2,750 ft per minute | |
SLS > 3,000 ft per minute | |
Service Ceiling | (ISA day) 19,1510 ft |
Hover Ceiling MRP-OGE | |
95°F 7,650 ft | |
70°F 9,375 ft | |
Standard Day 11,125 ft | |
Weight | Empty 11,516 Lbs |
Mission gross weight - 17,432 Lbs | |
Maximum gross weight - 22,000 Lbs | |
Maximum gross weight (ferry) - 24,500 Lbs | |
Length | 64 ft 10 in |
Height | 16 ft 10 in |
Rotor | Diameter 53 ft 8 in |
Four titanium and fiberglass blades Source: https://www.fas.org/man/dod-101/sys/ac/uh-60.htm |
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