请输入您要查询的百科知识:

 

词条 Chandelle Mk IV
释义

  1. Design and development

  2. Specifications (Mk IV)

  3. References

  4. External links

{{For|the flight maneuver|Chandelle}}
name=Mark IV image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft national origin=United States manufacturer=Chandelle Aircraft designer=Nile Downer first flight= introduced=1984 retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Chandelle Mk IV is an American ultralight aircraft that was designed by Nile Downer and produced by Chandelle Aircraft. The aircraft was supplied as a kit for amateur construction.[1][2]

Design and development

The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. The aircraft has a standard empty weight of {{convert|243|lb|kg|0|abbr=on}}. It features a strut-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.[1][2]

The aircraft is made from bolted-together aluminum tubing, with the wings and tail surfaces covered in Dacron sailcloth. Its tapered planform, single-surface, {{convert|30.5|ft|m|1|abbr=on}} span wing is supported by both lift struts and jury struts. The wing features 3/4 span ailerons. The pilot is accommodated in an open seat without a windshield. The tail surfaces are mounted on tubes that travel beside and below the pusher engine and propeller. The tricycle landing gear features main gear suspension.[1][2]

The Mark IV appeared just before the collapse of the US ultralight market in 1984 and so few were produced or sold.[1]

Specifications (Mk IV)

{{Aircraft specs
|ref=Cliche[1]
|prime units?=imp


|genhide=
|crew=one
|capacity=
|length m=
|length ft=17
|length in=
|length note=
|span m=
|span ft=30
|span in=6
|span note=
|height m=
|height ft=8
|height in=7
|height note=
|wing area sqm=
|wing area sqft=153
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=243
|empty weight note=
|gross weight kg=
|gross weight lb=500
|gross weight note=
|fuel capacity={{convert|5|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Cuyuna UL II-02
|eng1 type=twin cylinder, two-stroke engine
|eng1 kw=
|eng1 hp=30
|prop blade number=2
|prop name=wooden
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=59
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=45
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=23
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=75
|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=700
|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=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-4. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}
2. ^{{Cite web|url = http://virtualultralightmuseum.com/c.htm#chandelle|title = Chandelle Mk IV|accessdate = 2 December 2011|last = Virtual Ultralight Museum|date = n.d.}}

External links

  • Photo of a Mk IV

3 : United States ultralight aircraft 1980–1989|Homebuilt aircraft|Single-engined pusher aircraft

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/11 15:01:49