McDonnell Douglas MD530F: Difference between revisions
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*Max Range (no reserve): 232nm | *Max Range (no reserve): 232nm | ||
*Jet A-1: 5.56 Ibs/gallon | *Jet A-1: 5.56 Ibs/gallon | ||
=Gallery= | |||
<gallery mode=packed-hover> | |||
File:Weapong.png|Weapon Wing Loadout | |||
</Gallery> | |||
=Operators= | =Operators= |
Revision as of 20:44, 23 August 2017
McDonnell Douglas MD530F | ||||
---|---|---|---|---|
Type | Helicopter | |||
Passengers | 0 | |||
Crew | 2 | |||
Range | 232 nm | |||
Cruise Speed | 152 knots | |||
Fuel Capacity | 53.3 Imperial Gallons | |||
Takeoff Power | 650 shp | |||
Altitude Ceiling | 20,000 ft | |||
Engine Type | Turbine | |||
Engine Quantity | 1 | |||
Engine | Rolls-Royce Model M250-C30HU | |||
(v1.02) |
Notes
- Weapons Wing adds 51.7 Imperial Gallons to provide 111 Imperial Gallons
- Main Rotor Diameter: 26.4'
- Max Range (no reserve): 232nm
- Jet A-1: 5.56 Ibs/gallon
Gallery
- Weapong.png
Weapon Wing Loadout