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97:, 3,980 cc (242.9 cu in) displacement, air-cooled, direct drive gasoline engine design. It employs dual
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ignition and produces 90 kW (121 hp) for take-off at 2700 rpm, with a
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90 kW (121 hp) for takeoff, 80 kW (107 hp) continuous
386:
Unflown Wings: Soviet and
Russian Unrealised Aircraft Projects 1925-2010
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Model for limited aerobatics, to a maximum of 5 seconds inverted flight.
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Model for advanced aerobatics, including inverted flight.
334:, pages 258-259. Flying Pages Europe SARL, 2015.
8:
388:. Manchester: Créey Publishing. p. 472.
384:Gordon, Yefim; Komissarov, Sergey (2013).
166:Four cylinder, four stroke aircraft engine
332:World Directory of Light Aviation 2015-16
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193:3,980 cc (242.9 cu in)
73:(Letecke Opravny Malesice, Praha) of
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330:Tacke, Willi; Marino Boric; et al:
427:Air-cooled aircraft piston engines
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89:The engine is a four-cylinder
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432:2000s aircraft piston engines
199:1,052 mm (41.4 in)
220:105 kg (231.5 lb)
69:, designed and produced by
448:
422:LOM Praha aircraft engines
211:688 mm (27.1 in)
205:425 mm (16.7 in)
140:Phönix-Aviatechnica LKhS-4
184:115 mm (4.5 in)
175:105 mm (4.1 in)
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303:List of aircraft engines
158:General characteristics
154:Tacke and manufacturer
147:Specifications (M132A)
134:Fisher R-80 Tiger Moth
85:Design and development
364:www.pistovemotory.cz
280:Related development
266:Compression ratio
103:compression ratio
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405:Official website
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360:"M132A / M132AK"
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138:Considered for
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67:aircraft engine
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189:Displacement
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128:Applications
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358:LOM Praha.
253:Performance
91:four-stroke
77:for use in
416:Categories
309:References
231:Fuel type:
225:Components
216:Dry weight
340:1368-485X
152:Data from
142:(unbuilt)
71:LOM Praha
369:19 March
291:LOM M137
286:LOM M337
275:See also
233:gasoline
109:Variants
105:of 6.3.
60:LOM M132
209:Height:
197:Length:
99:magneto
95:in-line
338:
203:Width:
180:Stroke
120:M132AK
75:Prague
270:6.3:1
164:Type:
114:M132A
64:Czech
62:is a
25:Type
371:2018
336:ISSN
248:none
171:Bore
58:The
239:air
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362:.
346:^
317:^
93:,
81:.
373:.
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