Global Aircraft -- Proteus
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Proteus Specifications
Primary Function: |
Experimental - various functions |
Contractor: |
Scaled Composites |
Crew: |
2, single-pilot operation. Future models could be unmanned. |
Unit Cost: |
N/A |
Powerplant |
|
Two Williams Research/Rolls FJ44-2 turbofan engines, 2,300 lb thrust each |
Dimensions |
Length: |
56.3 ft |
Canard span: |
54.7 ft; 64.7 ft with removable tips installed |
Wingspan: |
77 ft, 7 in; 92 ft with removable tips installed |
Height: |
17.6 ft |
Weights |
Empty: |
5,900 lb |
Gross Takeoff: |
12,500 lb; 15,800 lb military usage |
Performance |
Speed: |
Mach 0.42 -- cruise; 280 kt at 40,000 ft |
Ceiling: |
65,000 ft at 7,000 lb |
Endurance: |
Up to 18 hr |
Armament |
|
N/A |
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Proteus Achievements
- The Proteus can be modified for almost any mission needed and can also be used as an UAV.
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