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The C90 is a Spanish, shoulder fired, 90 mm calibre, rocket-launcher weapon system, originally an anti-tank rocket launcher it has been upgraded and developed to be used in various combat roles, depending upon the fitted rocket warhead. The C90-C standard anti-tank model has an effective range of 200 metres and can penetrate 500 mm of armour (the original C90 could penetrate 250 mm) or 1200 mm of concrete. The C90-CR model can penetrate over 400 mm of armour, and the C90-CR-BK is fitted with a double charge warhead, a first charge penetrates the target and then the second charge, a fragmentation grenade, explodes inside the target to deal with the occupants.
Research C90

The Aermacchi MB 308 was an Italian two-seater light cabin monoplane of the 1950's supplied to both the Italian Air Force and supplied to the civilian market. The Aermacchi MB 308 was a high-wing cantilever monoplane of wooden construction powered by a Continental C85 or Continental C90 four-cylinder horizontally-opposed air-cooled engine providing a top speed of 197 kmh or203 k h respectively and a range of 760 km or 720 km respectively. A three-seater model, the Aermacchi MB 308G was also produced and a seaplane variant with twin floats fitted.
Research Aermacchi MB 308

The Aero Boero 95 is an Argentine three-seater light aircraft first flown as a prototype in 1959. The Aero Boero 95 is a braced high-wing monoplane of fabric-covered metal construction powered by one of several engines depending upon model. The Standard model is powered by a Continental C90-8F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 200 kmh and a range of 900 km. By 1970 a new version, the Aero Boero 95/115 was in production with a Lycoming O-235 engine providing a top speed of 210 kmh and a range of 800 km.
Research Aero Boero 95

The Alon Model A-2 AirCoupe is an American two-seater light aircraft developed as a refinement of the Ercoupe 415-C, and first flown in 1964. The Alon Model A-2 AirCoupe is a low-wing cantilever monoplane of all-metal construction powered by a Continental C90-16F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 208 kmh and a range of 730 km.
Research Alon Model A-2 AirCoupe

The Alpavia Jodel D117 Grand Tourisme is a French two-seat light monoplane first produced in 1959. The Alpavia Jodel D117 is a low-wing cantilever monoplane of fabric covered wood construction powered by a Continental C90-14F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 207 kmh and a range of 1170 km.
Research Alpavia Jodel D117

The C.A.B. YG-30 Supercab was a French two-seater dual-control light aircraft of the 1950's developed from the earlier C.A.B. GY-20, and first flown in 1954. The C.A.B. YG-30 was a low-wing cantilever monoplane of wooden construction powered by a Continental C90 four-cylinder horizontally-opposed air-cooled engine providing a top speed of 275 kmh.
Research C.A.B. YG-30

The Centre Est-Jodel DR100 Ambassadeur is a French three-seater light touring monoplane. The Centre Est-Jodel DR100 Ambassadeur is a low-wing cantilever monoplane of wooden construction powered by a Continental C90-14F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 210 kmh and a range of 1170 km.
Research Centre Est-Jodel DR100 Ambassadeur

The Jodel-Wassmer D 120 Paris-Nice is a French two-seat side-by-side light cabin monoplane with dual controls, developed as a deluxe version of the Jodel D112, and first flown as a prototype in 1955. The D 120 is powered by a Continental C90-12F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 210 kmh and a range of 1100 km.
Research D 120

The Putzer Elster is a German two-seater light monoplane. The Elster is a braced high-wing monoplane of plywood and metal construction originally powered by a Porsche 678/3 four-cylinder horizontally-opposed air-cooled engine providing a top speed of 140 kmh and a range of 650 km. A later B model was produced powered by a Continental C90-12F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 168 kmh and a range of 450 km. In 1966 A C model powered by a Lycoming O-320 engine was produced for use as a glider tug.
Research Elster
The Fornaire Execta is an American two-seater light monoplane first flown in 1956. The Fornaire Execta is a low-wing cantilever monoplane of metal construction powered by a Continetal C90-12F four-cylinder horizontally-opposed air-cooled engine providing a top cruising speed of 194 kmh and a range of 805 km.
Research Fornaire Execta
 
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The Probert Encyclopaedia was designed, edited and programed by
Matt and Leela Probert
©1993 - 2009 The Probert Encyclopaedia
Southampton, United Kingdom
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