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词条 Brochet MB.70
释义

  1. Design and development

  2. Variants

  3. Units using this aircraft

  4. Specifications (MB.72)

  5. References

name=MB.70 Seriesimage=Brochet MB.76 Chavenay 04.06.67.jpgcaption=The Brochet MB.76 at Chavenay airfield near Paris in June 1967

}}{{Infobox Aircraft Type

type=Sports planemanufacturer=Brochetdesigner=Maurice Brochetfirst flight=28 January 1950introduced=retired=status=primary user=more users=produced=number built=8variants with their own articles=
}}

The Brochet MB.70 was a two-seat light aircraft developed in France in the early 1950s for recreational flying and amateur construction.

Design and development

It was a high-wing braced monoplane of conventional configuration that seated the pilot and passenger in tandem within a fully enclosed cabin. It was fitted with fixed tailwheel undercarriage layout and was of all-wooden construction. Progress was hastened by the publication of a Service de l'Aviation Légère et Sportive requirement for a new light aircraft for French aeroclubs, and a series of development machines were built with a variety of different engines, eventually leading to the definitive Brochet MB.80.[1]

Variants

  • MB.70 - prototype powered by Salmson 9Adb radial (1 built)
  • MB.71 - version with Minie 4DC-32 engine (1 built)
  • MB.72 - version with Continental A65 horizontally opposed four-cylinder engine (5 built)
  • MB.73 - version with Continental A65-85 horizontally opposed four-cylinder engine (1 converted from the MB.70)
  • MB.76 - version with Continental C90-14F horizontally opposed four-cylinder engine (1 built)

Units using this aircraft

Private and club pilots

Specifications (MB.72)

{{aerospecs
|met or eng?=met
|crew=One pilot
|capacity=1 passenger
|length m=6.68
|length ft=21
|length in=11
|span m=10.35
|span ft=33
|span in=11
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.5
|height ft=8
|height in=2
|wing area sqm=14.0
|wing area sqft=151
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=366
|empty weight lb=807
|gross weight kg=570
|gross weight lb=1,257
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Continental A65
|eng1 kw=48
|eng1 hp=65
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=130
|max speed mph=81
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

References

{{commons category|Brochet MB.70}}
Notes
1. ^Simpson, 2005, p.71
Bibliography
{{refbegin}}
  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=215 }}
  • {{cite book |title=World Aircraft Information Files |publisher=Bright Star Publishing|location=London |pages=File 890 Sheet 99 }}
  • {{cite book |last= Simpson |first=Rod|title=The General Aviation Handbook|year=2005 |publisher=Midland Publishing|isbn=1-85780-222-5}}
{{refend}}{{aircontent
|related=
|similar aircraft=
|lists=
|see also=
}}{{Brochet aircraft}}

5 : French sport aircraft 1950–1959|Brochet aircraft|High-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1950

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