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词条 Warwick M-1 Tiny Champ
释义

  1. Design and development

  2. Specifications (M-1 Tiny Champ)

  3. References

  4. External links

name=M-1 Tiny Champ image= caption=

}}{{Infobox Aircraft Type

type=Homebuilt aircraft national origin=United States manufacturer= designer=Bill Warwick first flight=1 May 1960 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost=$1,200 developed from= variants with their own articles=
}}

The Warwick M-1 Tiny Champ is an American homebuilt aircraft that was designed by Bill Warwick

and first flown on 1 May 1960.

Design and development

The M-1 is a single engine, strut-braced, high wing, open cockpit, conventional landing gear-equipped aircraft. Doors and a rear window can be installed to create an enclosed cabin.[1] The design won outstanding aircraft design at the Experimental Aircraft Association Airshow in 1960.[2]

Specifications (M-1 Tiny Champ)

{{Aircraft specs
|ref=Flying Magazine
|prime units?=kts


|genhide=
|crew=1
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=20
|span in=
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|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Continental A65
|eng1 type=horizontally opposed piston aircraft engine
|eng1 kw=
|eng1 hp=65
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|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=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|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=
|avionics=
}}

References

1. ^{{cite journal|magazine=Flying|date=November 1960|title=Experimental Aircraft Fly-In|volume=67|issue=5|page=36|url=https://books.google.com/books?id=nt0RgQ2RqTgC&lpg=PA36&dq=Warwick%20Tiny%20Champ&pg=PA36#v=onepage&q=Warwick%20Tiny%20Champ&f=false}}
2. ^{{cite web|title=Steen Aero|url=http://www.steenaero.com/articles_detail.cfm?PrintFriendly=1&ArticleID=27|accessdate=1 October 2014}}

External links

  • Image of the W-1

1 : Homebuilt aircraft

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