HCSL-12
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Revision as of 22:24, 27 May 2007 by Waterhelper (Talk | contribs)
HCSL-12 Strategic cargo lifter | |||
General characteristics | |||
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Crew: | 8 typical (Pilot, first pilot, copilot, two flight engineers, three loadmasters) 4 minimum (Pilot, copilot, two flight engineers) | ||
Payload: | 150,000kg | ||
Length: | 80 m | ||
Wingspan: | 73.2m | ||
Height: | 21m | ||
Wing area: | 600 m² | ||
Empty weight: | 175,000 kg | ||
Max takeoff weight | 400,000kg | ||
Powerplant | FHPTE-4 x4 | ||
cost | 180 million universal dollars | Performance | |
Maximum speed: | Mach 0.84 | ||
Cruise speed: | Mach 0.78 | ||
Range: | 2,750 | ||
Service ceiling: | 15,000m | ||
Rate of climb: | 11.45 m/s | ||
Wing loading: | 625 kg/m² | ||
Thrust/weight: | 0.43 | ||
Takeoff roll: | 2,550m | ||
Landing Roll: | 1,025m | ||
Fuel capacity: | 210,453l |