the specifications:
Primary Function: experimental - Laminar Flow Research
Aircraft
Contractor: General Dynamics Corp.
Crew: One
Unit Cost: N/A
Powerplant: Pratt and Whitney 100-PW-100 engine (with afterburner),
rated at 23,830 lb thrust
Length: 54.2 ft (16.52 m)
Wingspan: 34.3 ft (10.45 m)
Height: 17.7 ft (5.39 m)
Weights
Empty: N/A
Max. Weight: 48,000 lb (17,915.60 kg)
Performance
Speed: Mach 1.8 (1,260 mph)
Ceiling: 50,000 ft
Range: 2,850 miles
Armament
N/A
