|Microjet 200 prototype at Farnborough Airshow in 1982.|
|Role||Lightweight jet trainer|
|First flight||24 June 1980|
Design and development
Designed by Microjet SA, as a vehicle for the small gas turbine engines produced by Microturbo and as a two-seat lightweight jet trainer. The 200 is a low-wing cantilever monoplane with a retractable tricycle landing gear and a v-tail. It is powered by two Microturbo TRS 18-1 turbojets. It had side-by-side seating for an instructor and student. The all-wood prototype 200 first flew on 24 June 1980. Three pre-production aircraft designated 200B were built of mixed construction and the first flew on 19 May 1983. The third had small winglets on the tail. The project failed to gain any interest and no production aircraft were built.
- Prototype, one built.
- Pre-production, three built.
Data from Jane's All The World's Aircraft 1988-89 
- Crew: 2
- Length: 6.67 m (21 ft 10½ in)
- Wingspan: 7.56 m (24 ft 9¾ in)
- Height: 2.42 m (7 ft 11¼ in)
- Wing area: 6.12 m2 (65.9 ft2)
- Empty weight: 780 kg (1,719 lb)
- Gross weight: 1,300 kg (2866 lb)
- Powerplant: 2 × Microturbo TRS 18-1 turbojet engines, 1.30 kN (293 lbf) thrust each
- Maximum speed: 463 km/h (287 mph)
- Cruising speed: 389 km/h (241 mph)
- Endurance: 2 hours
- Service ceiling: 9,150 m (30,000 ft)
- Rate of climb: 8.7 m/s (1,705 ft/min)
|Wikimedia Commons has media related to Microturbo Microjet 200.|
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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