Flat Wing Area
88.2579 m²
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All data (22 fields)
- Name
- Northrop YF-23
- Manufacturer
- Northrop Corporation
- Description
- The Northrop–McDonnell Douglas YF-23 is an American single-seat, twin-engine, stealth fighter prototype technology demonstrator designed for the United States Air Force (USAF).
- First Flight
- 1990-08-27
- Production End
- 1990-01-01
- Designer
- Northrop Corporation
- Type
- Stealth fighter prototype Technology demonstrator
- Length (m)
- 20.4216
- Height (m)
- 3.9624
- Cockpit Crew
- 1
- Max Ceiling (m)
- 19800
- Armament
- None as tested but provisions made for:; 1 × 20 mm (0.79 in) M61 Vulcan cannon; 4 × AIM-120 AMRAAM or AIM-7 Sparrow medium-range air-to-air missiles; 2 × AIM-9 Sidewinder short-range air-to-air missiles
- Max Mach (Mach)
- 2.2
- National Origin
- United States of America
- Number Built
- 2
- Powerplant Description
- 2 × Pratt & Whitney YF119-PW-100N or General Electric YF120-GE-100N afterburning turbofans
- Primary Users
- United States Air Force
- Status
- Canceled
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Northrop_YF-23
- Flat Wing Span (m)
- 13.1064
- Flat Wing Area (m²)
- 88.2579
- Number of Engines
- 2