Armstrong Whitworth A.W.52
Flat Wing Area
122.0746 m²
Maximum Range
2414.016 km
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All data (23 fields)
- Name
- Armstrong Whitworth A.W.52
- Manufacturer
- Armstrong Whitworth
- Description
- The Armstrong Whitworth A.W.52 was an early flying wing aircraft designed and produced by British aircraft manufacturer Armstrong Whitworth Aircraft.
- First Flight
- 1947-11-13
- Service End
- 1954-01-01
- Designer
- John Lloyd
- Type
- Experimental flying wing
- Length (m)
- 11.4
- Height (m)
- 4.4
- Cockpit Crew
- 2
- Max Speed (km/h)
- 804.672
- Max Ceiling (m)
- 10972.8
- Rate of Climb (m/s)
- 24.384
- Capacity Description
- 4000 lb / 300 cuft
- National Origin
- United Kingdom
- Number Built
- 2
- Powerplant Description
- 2 × Rolls-Royce Nene centrifugal-flow turbojet
- Primary Users
- Royal Aircraft Establishment
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Armstrong_Whitworth_A.W.52
- Flat Wing Span (m)
- 27.4
- Flat Wing Area (m²)
- 122.0746
- Aircraft Engine
- Rolls-Royce Nene
- Number of Engines
- 2