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词条 Magni Vale
释义

  1. Design and development

  2. Variants

  3. Specifications (Vale)

  4. References

     Notes  Bibliography 
name=Magni Vale image=Magni PM-3-4 Vale, Museo Nazionale della Scienza e della Tecnologia (Milan).jpg caption= The only Magni Vale on display at Museo della Scienza e della Tecnologia "Leonardo da Vinci", Milan, Italy

}}{{Infobox Aircraft Type

type=Monoplane tourer and aerobatic trainer national origin=Italy manufacturer=Piero Magni-Aviazione designer=Piero Magni first flight=1930s introduced= retired= status= primary user= number built=1 developed from= variants with their own articles=
}}

The Magni Vale PM-3-4 was an Italian civil monoplane for use as a tourer or aerobatic trainer designed and built by Piero Magni-Aviazione in Milan.

Design and development

The Vale was a sleek single-seat parasol wing braced monoplane powered by a {{convert|130|hp|kW|0|abbr=on}} Farina T.58 radial engine. An improved variant, the Supervale PM-4-1 had a {{convert|140|hp|kW|0|abbr=on}} Fiat A.54 engine. The start of the second world war halted design and development by the company.

Variants

Vale PM-3-4

Powered by a {{convert|130|hp|kW|0|abbr=on}} Farina T.58 radial engine.

Supervale PM-4-1

Powered by a {{convert|140|hp|kW|0|abbr=on}} Fiat A.54 engine.

Specifications (Vale)

Performance figures calculated

{{Aircraft specs
|ref=Les Ailes 7 February 1935
|prime units?=met


|genhide=
|crew=One
|length m=5.50
|length note=
|span m=8.90
|span note=
|height m=2.02
|height note=
|wing area sqm=10.69
|aspect ratio=
|airfoil=
|empty weight kg=540
|empty weight note=
|gross weight kg=765
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Farina T.58
|eng1 type=5-cylinder radial engine
|eng1 hp=130
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=ground adjustable pitch


|perfhide=
|max speed kmh=250
|max speed note=
|cruise speed kmh=200
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=90
|minimum control speed note=
|range km=1000
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=7000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

Notes


}}

Bibliography

{{refbegin}}
  • {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}}

3 : Italian civil utility aircraft 1930–1939|Single-engined tractor aircraft|Parasol-wing aircraft

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