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User:Cedar T./UH-60 - weights and measures

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Specifications (UH-60L)

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Orthographically projected diagram of the UH-60A Black Hawk.
Orthographically projected diagram of the UH-60A Black Hawk.
Drawing from Army manual
Aeromedical configuration

Data from Encyclopedia of Modern Warplanes,[1] US Army Fact File,[2] International Directory,[3] Black Hawk,[4] Globalsecurity.org[5][6]

General characteristics

  • Crew: 3-4 (pilot, copilot, 1 or more crew chiefs/gunners)
  • Capacity: 2,640 lb of cargo internally, including 11 troops or 6 stretchers, or 9,000 lb of cargo externally
  • Length: 64 ft 10 in ([convert: unknown unit])
  • Wingspan: 53 ft 8 in (16.36 m)
  • Height: 16 ft 10 in (5.13 m)
  • Wing area: 2,260 sq ft (210 m2)
  • Empty weight: 11,516 lb (5,224 kg)
  • Gross weight: 17,432 lb (7,907 kg)
  • Max takeoff weight: 22,000 lb ([convert: unknown unit])
  • Powerplant: 2 × General Electric T700-GE-701C turboshaft, 1,890 hp (1,410 kW) each

Performance

  • Maximum speed: 183 mph (295 km/h, 159 kn)
  • Cruise speed: 173 mph (278 km/h, 150 kn)
  • Never exceed speed: 222 mph (357 km/h, 193 kn)
  • Combat range: 368 mi (592 km, 320 nmi)
  • Ferry range: 1,380 mi (2,220 km, 1,200 nmi) with ESSS stub wings and external tanks[4]
  • Service ceiling: 19,000 ft (5,790 m)
  • Rate of climb: 700 ft/min (3.6 m/s)
  • Wing loading: 7.19 lb/sq ft (35.4 kg/m2)
  • Power/mass: 0.192 hp/lb (158 W/kg)

Armament

References

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  1. ^ a b Gunston, Bill (1995). The Encyclopedia of Modern Warplanes. London: Aerospace Publishing Ltd. ISBN 1-56619-908-5.
  2. ^ "Black Hawk". US Army Fact Files.
  3. ^ Frawley, Gerald. The International Directory of Military Aircraft, 2002/2003. Aerospace Publications, 2002. ISBN 1-875671-55-2.
  4. ^ a b c d e f g h Tomajczyk 2003, pp. 11, 14–15.
  5. ^ "UH-60L / S-70A Blackhawk". GlobalSecurity.org. Retrieved 26 January 2011.
  6. ^ "UH-60L Black Hawk". GlobalSecurity.org. Retrieved 26 January 2011.
  7. ^ "Self-Defense Armament Subsystem M240H Aviation Machine Gun" (PDF). U.S. Army PEO Soldier. Retrieved 22 November 2010.

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