Specifications (CL-1200-2 / X-27)
Data from NB: These are estimated figures given by Lockheed as neither type flew.
General characteristics
- Crew: One
- Length: 57 ft 3 in / 53 ft 2 in (17.45 / 16.2 m)
- Wingspan: 29 ft 2 in / 28 ft 7 in (8.89 / 8.7 m)
- Height: 17 ft 2 in / 16 ft 2 in (5.23 / 4.9 m)
- Wing area: 300 ft² (28 m²)
- Airfoil: Bi-convex
- Empty weight: 17,885 / 17,250 lb (8,112/ 7,800 kg)
- Loaded weight: 24,385 / 32,500 lb (11,061 / 16,000 kg)
- Max. takeoff weight: 35,000 lb (15,900 kg)
- Powerplant: 1 × Pratt & Whitney TF30-P-100 turbofan
- Dry thrust: 15,000 lbf (66.7 kN)
- Thrust with afterburner: 25,000 lbf (111.2 kN)
Performance
- Maximum speed: 1,477 / 1,260 kn at 35,000 ft (Mach 2.57 / 2.19) (1,700 / 1,450 mph, 2,720 / 2,330 km/h)
- Range: 367 nmi combat radius with 4,000 lb (8,800 kg) bombload / 1,836 nmi range (420 / 2,100 mi, 680 / 3,400 km)
- Service ceiling: In excess of 60,000 ft (>18,300 m)
- Rate of climb: 60,000ft/min (300m/s)
- Takeoff run: 1,450 ft (440 m)
- Landing run: 2,060 ft (930 m)
Armament
CL-1200-2 only:
- 1 × 20 mm General Electric M61 Vulcan cannon with 725 rounds, or
- 1 × 30 mm DEFA cannon with 400 rounds
- Up to 12,000 pounds (5,400 kg) ordnance
Read more about this topic: Lockheed CL-1200