Armstrong Whitworth Atlas

Airplanes

Length

8.5344 m

Flat Wing Span

11.8872 m

Height

3.048 m

Flat Wing Area

36.3251 m²

Max Speed

228.5268 km/h

Max Ceiling

5120.64 m

Number of Engines

Aircraft Engine

First Flight

1925-05-10

Entry Into service

1927-01-01

Number Built

478

Maximum Take-Off Weight

1.8234 t (paragliders: kg)

Maximum Range

643.7376 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Armstrong Whitworth Atlas	1.8234	643.7376

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aermacchi AL-60		8.79	11.84	8	Compare
Aermacchi AM.3		8.73	11.73		Compare
Auster Agricola	Continental O-470	8.5344	12.8016	2	Compare
Berliner-Joyce P-16		8.59	10.36		Compare
Bristol Type 133	Bristol Mercury	8.53	11.89		Compare
Aviones de Colombia AC-05 Pijao		8.09	12.63		Compare

All data (24 fields)

Name: Armstrong Whitworth Atlas
Manufacturer: Armstrong Whitworth
Description: The Armstrong Whitworth Atlas was a British single-engine biplane designed and built by Armstrong Whitworth Aircraft.
First Flight: 1925-05-10
Entry Into service: 1927-01-01
Production End: 1933-01-01
Service End: 1935-01-01
Designer: Armstrong Whitworth
Type: Army cooperation aircraft
Length (m): 8.5344
Height (m): 3.048
Cockpit Crew: 2
Max Speed (km/h): 228.5268
Max Ceiling (m): 5120.64
Armament: 1 × forward firing .303 in (7.7 mm) Vickers machine gun and 1 × .303 in (7.7 mm) Lewis Gun on Scarff ring in rear cockpit; Up to 4 × 112 lb (51 kg) bombs under wings
Endurance (h): 3
Number Built: 478
Powerplant Description: 1 × Armstrong Siddeley Jaguar IVC 14-cylinder two-row air-cooled radial engine, 336 kW (450 hp) each
Primary Users: Royal Air Force, Royal Canadian Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Armstrong_Whitworth_Atlas
Flat Wing Span (m): 11.8872
Flat Wing Area (m²): 36.3251
Aircraft Engine: Armstrong Siddeley Jaguar
Number of Engines: 1