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Military




UH-60A Black Hawk

Specifications
Model UH-60A
Manufacturer Sikorsky Aircraft
Folded Length (rotor/tail pylon)40 ft, 11in
Rotor folded length (pylon flight position)53 ft, 3 in
Length overall (rotors turning)64 ft, 10 in / 19.76m
Fuselage length 50 ft / 15.26m
Height: (to top of rotor) head3.79m
Overall height, (tail rotor turning)17 ft / 5.18m
Fuselage width 7 ft, 9 in / 2.36m
Folded width 10 ft, 7 in
Main rotor diameter 53 ft, 8 in / 16.36m
Main rotor blade chord 0.53m
Tail rotor diameter 11 ft / 3.35m
Ground clearance 11.2 in
Ground to tail rotor clearance6 ft, 8 in
Turning radius 41 ft, 7 in
Clearance for 180° 84 ft
Areas
Main rotor disc 210.15m2
Tail rotor disc 8.83m2
Vertical fin 3.00m2
Horizontal tail surfaces 4.18m2;
Weights and Loadings
Weight empty (ASW) 6.191kg
Mission fuel load (usable)
Maximum useful load (fuel and disposable ordinance)
Maximum takeoff and landing weight
Maximum disc loading 47.2kg/m2
Maximum power loading 3.92kg/m2
Performance
Never-exceed speed (Vne)
Maximum level speed at S/L (Dash Speed)126 knots
Rate of climb at S/L, OEI 213m/min
Service ceiling 5,790m
Service ceiling, OEI 21287
Hovering ceiling 2,895mIGE
Range at S/L with standard fuel, no reserves319 nm



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