Flat Wing Area
162.1158 m²
Cruise Speed
540.7835 km/h
Entry Into service
1956-12-01
Maximum Take-Off Weight
70.3068 t (paragliders: kg)
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All data (25 fields)
- Name
- Lockheed C-130 Hercules
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed C-130 Hercules is an American, four-engined, turboprop, military transport aircraft designed and built by Lockheed (now Lockheed Martin).
- First Flight
- 1954-08-23
- Entry Into service
- 1956-12-01
- Designer
- Lockheed Corporation
- Type
- Tactical airlifter
- Length (m)
- 29.5656
- Height (m)
- 11.5824
- Cockpit Crew
- 5
- Max Speed (km/h)
- 592.6395
- Cruise Speed (km/h)
- 540.7835
- Max Ceiling (m)
- 10058.4
- Rate of Climb (m/s)
- 9.2964
- Capacity Description
- 42000 lb payload; C-130E/H/J cargo hold: length, 40 ft; width, 9 ft; height, 9 ft. Rear ramp: length, 123 in; width, 119 in; C-130J-30 cargo hold: length, 55 ft; width, 9 ft; height, 9 ft. Rear ramp:…
- National Origin
- United States of America
- Number Built
- 2700
- Powerplant Description
- 4 × Allison T56-A-15 turboprop engines, 3423 kW (4590 hp) each
- Primary Users
- United States Air Force, United States Navy, United States Coast Guard, United States Marine Corps
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_C-130_Hercules
- Flat Wing Span (m)
- 40.2336
- Flat Wing Area (m²)
- 162.1158
- Aircraft Engine
- Allison T56
- Number of Engines
- 4