SIPA S.200 Minijet

1952

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SIPA S.200 Minijet

The SIPA 200 Minijet was a single-engined, turbojet-powered two-seat training and liaison aircraft. It was distinctive in its twin-boom configuration and short, tubby nacelle housing the engine and cockpit. The S.200 made its first flight on 14 January 1952. Early test flights revealed that it was underpowered and performance fell short of expectations, and it was unable to compete with contemporary types such as the Fouga Magister. Seven prototypes were built. The SIPA 200 was built at the request of the French government, which was evaluating new aviation concepts as part of the progressive build-up of France's postwar aircraft industry.

3-View 
SIPA S.200 MinijetA three-view drawing (588 x 438)

Specification 
 CREW2
 ENGINE1 x 150kg Turbomeca Palas turbojet engine
 WEIGHTS
  Take-off weight780 kg1720 lb
  Empty weight450 kg992 lb
 DIMENSIONS
  Wingspan7.20 m24 ft 7 in
  Length5.12 m17 ft 10 in
  Height1.78 m6 ft 10 in
  Wing area9.6 m2103.33 sq ft
 PERFORMANCE
  Max. speed400 km/h249 mph
  Ceiling8000 m26250 ft
  Range500 km311 miles

SIPA S.200 Minijet

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ubaTaeCJ, e-mail, 21.11.2024 12:06

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ubaTaeCJ, e-mail, 21.11.2024 12:02

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ubaTaeCJ, e-mail, 21.11.2024 12:01

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ubaTaeCJ, e-mail, 21.11.2024 11:58

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ubaTaeCJ, e-mail, 21.11.2024 11:43

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