Brochet MB.100
| MB.100 | |
|---|---|
| Role | Sports plane |
| Manufacturer | Brochet |
| Designer | Maurice Brochet |
| First flight | 3 January 1951 |
| Number built | 21 |
|
| |
The Brochet MB.100 was a three-seat light aircraft developed in France in the early 1950s.
Design and development
A further derivative of the Brochet MB.70, the MB.100 uses essentially the same airframe as the MB.80, but with a revised tail and cabin, the latter now including a third seat. Service de l'Aviation Légère et Sportive purchased several examples for distribution to French aeroclubs, including a number of tropicalised versions for use in North Africa. Unlike its predecessors, the MB.100 was not designed for homebuilding.
Variants
- MB.100 - initial production version (7 built)
- MB.101 - tropicalised version with engine air filter and more durable exterior finish (14 built)
Specifications (MB.100)
General characteristics
- Crew: One pilot
- Capacity: 2 passengers
- Length: 6.50 m (21 ft 4 in)
- Wingspan: 10.65 m (34 ft 11 in)
- Height: 2.00 m (6 ft 7 in)
- Wing area: 14.4 m2 (155 ft2)
- Empty weight: 465 kg (1,025 lb)
- Gross weight: 780 kg (1,720 lb)
- Powerplant: 1 × Hirth HM 504A-2, 75 kW (100 hp)
Performance
- Maximum speed: 180 km/h (112 mph)
- Range: 600 km (374 miles)
- Service ceiling: 3,500 m (11,480 ft)
References
 |
Wikimedia Commons has media related to Brochet. |
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 215.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 99.
- Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 100–01.
This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.