Sikorsky UH-60 Black Hawk
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Explore the Sikorsky UH-60 Black Hawk in side view and top view to compare its silhouette and proportions.


From Wikipedia
The Sikorsky UH-60 Black Hawk is a four-blade, twin-engine, medium-lift military utility helicopter manufactured by Sikorsky Aircraft. Sikorsky submitted a design for the United States Army's Utility Tactical Transport Aircraft System (UTTAS) competition in 1972. The Army designated the prototype as the YUH-60A and selected the Black Hawk as the winner of the program in 1976, after a fly-off competition with the Boeing Vertol YUH-61.
Summary of “Sikorsky UH-60 Black Hawk” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Sikorsky UH-60 Black Hawk by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/H60/), CC BY 4.0Specifications
- Length
- 19.51 m64 ft
- Rotor diameter
- 16.15 m53 ft
- Max take-off weight
- 9.98 t22,000 lb
- Cruise speed
- 282 km/h175 mph
- Max speed
- 294 km/h183 mph
- Range
- 511 km318 mi
- Ceiling
- 5,791 m19,000 ft
- Engines
- 2× GE T700 (turboshaft)
- Power
- 2× 1 902 hp
- First flight
- 1974
- In service
- 1979
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.



