Mauboussin M.200

The Mauboussin M.200 was a French racing monoplane built by Fouga. It was a low-wing cantilever monoplane with a fixed tailskid landing gear. It had an enclosed cockpit for a pilot, and was powered by a Régnier 85.8 kW (115 hp) 4E.0 engine. It first flew on 21 March 1939, and in May 1939 established new FAI records for an aircraft of its class.

Mauboussin M-200
Role	Racing monoplane
Manufacturer	Fouga
First flight	21 March 1939
Number built	3

Variants

M.200

The first prototype of a single-seat training / racing aircraft, powered by a 71 kW (95 hp) Régnier 4E.0 inverted air-cooled in-line piston engine, first flown on 21 March 1939.

M.201

A second airframe produced and supposed to be powered by a 110 kW (150 hp) Régnier 4E.0.

M.202

A second flyable prototype which might use the airframe of M.201 powered by a 71 kW (95 hp) Régnier 4E.0, first flown in June 1941.

Specifications

Mauboussin M.202 3-view drawing from L'Aerophile July 1942

Data from

General characteristics

• Length: 6.92 m (22 ft 8 in)
• Wingspan: 7.28 m (23 ft 11 in)
• Height: 2.25 m (7 ft 5 in)
• Wing area: 7.5 m² (81 sq ft)
• Empty weight: 370 kg (816 lb)
• Gross weight: 578 kg (1,274 lb)
• Powerplant: 1 × Régnier 4Eo 4-cyl. air-cooled inverted in-line piston engine, 71 kW (95 hp)

Performance

• Maximum speed: 285 km/h (177 mph, 154 kn)
• Range: 1,000 km (620 mi, 540 nmi)
• Service ceiling: 6,000 m (20,000 ft)

Bibliography

• Parmentier, Bruno. "Mauboussin M-200" (in French). Retrieved 10 March 2014.
• Parmentier, Bruno. "Mauboussin M-201" (in French). Retrieved 10 March 2014.
• Parmentier, Bruno. "Mauboussin M-202" (in French). Retrieved 10 March 2014.
• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2435

External links

• Aviafrance article in French