79:, featuring a single-speed supercharger. The 122 R.C.38 major production variant had a reduction gearbox, single stage supercharger and rated altitude of 3,800 m (12,500 ft).
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was a 12-cylinder inverted-V aircraft engine produced in 1941 by Alfa Romeo Milano as a licence-built
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Archivio
Storico Alfa Romeo - Volume II. Torino, novembre 1998.
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368 kW (493 hp) at 3,800 m (12,500 ft)
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Centrifugal compressor, diameter 210 mm (8.3 in)
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129:18.6 L (1,135.04 cu in)
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438:Air-cooled aircraft piston engines
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453:Inverted V12 aircraft engines
448:1930s aircraft piston engines
135:1,790 mm (70.5 in)
443:Alfa Romeo aircraft engines
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147:781 mm (30.7 in)
141:725 mm (28.5 in)
220:de Havilland Gipsy Twelve
120:140 mm (5.5 in)
111:118 mm (4.6 in)
98:60° 12-cylinder inverted
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257:List of aircraft engines
90:General characteristics
225:Isotta Fraschini Gamma
192:Related development
204:Comparable engines
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102:air-cooled engine
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230:Junkers Jumo 210
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31:aircraft engine
19:Alfa Romeo 122
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83:Specifications
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77:Walter Sagitta
70:Alfa Romeo 122
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61:Walter Sagitta
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56:Developed from
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316:aero engines
268:Bibliography
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215:Argus As 411
210:Argus As 410
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240:Renault 12R
174:Performance
169:Air cooling
432:Categories
313:Alfa Romeo
152:Components
47:First run
41:Alfa Romeo
397:Mercurius
187:See also
407:RA 1050
402:RA 1000
387:Jupiter
145:Height:
133:Length:
139:Width:
116:Stroke
28:Piston
263:Notes
96:Type:
50:1941
24:Type
392:Lynx
107:Bore
100:V-12
68:The
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332:D2
305:e
298:t
291:v
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