Maximum Take-Off Weight
15.9 t (paragliders: kg)
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Aircraft Weight Variants
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All data (20 fields)
- Name
- Lockheed CL-1200 Lancer
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed CL-1200 Lancer was a late 1960s company-funded proposal for a fighter aircraft based on the Lockheed F-104 Starfighter.
- Designer
- Lockheed Corporation
- Type
- Interceptor
- Length (m)
- 17.45
- Height (m)
- 5.23
- Max Speed (km/h)
- 2720
- Max Ceiling (m)
- 18288
- Rate of Climb (m/s)
- 300
- 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 12000 lb ordnance
- Max Mach (Mach)
- 2.57
- National Origin
- United States of America
- Powerplant Description
- 1 × Pratt & Whitney TF30-P-100 turbofan, 66.7 kN thrust each
- Status
- Cancelled at mock-up stage
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_CL-1200_Lancer
- Flat Wing Span (m)
- 8.89
- Flat Wing Area (m²)
- 28
- Aircraft Engine
- Pratt & Whitney TF30
- Number of Engines
- 1