C-130B Hercules
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In 1951 USAF submitted to Boeing Co., Douglas, Fairchild and Lockheed
a request for building a tactical transport aircraft. The new aircraft
had to be capable of short take-off and landing, to transport at
least 92 combat ready personnel or 64 paratroopers up to 2100 km,
or 30000 kg load up to 1800 km. It also had to have two side doors
and a rear hatch capable of in-flight use.
Technical data
Powerplant: four Allison T-56A turboprop engines. Dimensions: - Length: 29,8m; - Height: 11,66m; - Wingspan: 40,41m. Weights:: - empty: 34686kg; - Normal takeoff weight: 70310kg; - Maximum takeoff weight: 79380kg. Weapons: - none. Payload: 18000kg (92 combat ready troops or 68/84 paratroopers) Crew: 5. Performance: - Maximum sped at ground level: 616km/h; - Cruising speed: 528km/h; - Ceiling: 10000m; - Maximum range: 5200km.
C-130B Hercules |
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