McDonnell Douglas C-17 Globemaster III
1991
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McDonnell Douglas C-17 Globemaster III

The first prototype flew in September 1991. Entered service in 1994.

McDonnell Douglas C-17 Globemaster III


Specification 
 CREW3
 ENGINE4 x P+W F117-PW-100, 185.5kN
 WEIGHTS
    Take-off weight265306 kg584903 lb
 DIMENSIONS
    Wingspan51.8 m169 ft 11 in
    Length53.0 m173 ft 11 in
    Height16.8 m55 ft 1 in
 PERFORMANCE
    Cruise speed820 km/h510 mph
    Range8710 km5412 miles
    Range w/max.payload4456 km2769 miles

Comments 
R Ganesh, rganesh(@)sp.edu.sg, 20.11.2008

I don't have a comment but a question. What is the lift off velocity of the C17 Globemaster 3, i.e., speed at which lift just equals weight?

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