请输入您要查询的百科知识:

 

词条 Birdman Project 102
释义

  1. Development

  2. Specifications (Project 102)

  3. References

name=Project 102 image= caption=

}}{{Infobox Aircraft Type

type=Ultralight motor glider national origin=Canada manufacturer=Birdman Enterprises designer=Dr David Marsden first flight=1982 introduced= retired= status=Experimental primary user= number built=1 developed from= variants with their own articles=
}}

The Birdman Project 102, also known as Windsoar, was an experimental high wing, single engine, pod-and-boom, conventional landing gear-equipped, ultralight motor glider originally intended for production by Birdman Enterprises.[1]

Development

Project 102 was intended to result in a production lightweight motor glider and was designed in 1981 by David Marsden from the University of Alberta with assistance from Birdman Enterprises' designer Vladimir Talanczuk. The production aircraft was tentatively named the Birdman Windsoar.[1]

The Project 102 aircraft was built from aluminum and foam. The all-metal wing was cantilever, stressed to +6/-6 g and featured full-span reflexing ailerons that could be raised to increase cruise performance, as well as winglets. The wing centre was covered with aircraft fabric. The cockpit included a windshield, with the sides left open, although a full enclosure was intended to be optional. The conventional low tail was mounted on a long aluminum tail boom.[1]

The single engine was in pusher configuration and was planned for {{convert|10|to|25|hp|kW|0|abbr=on}}.[1]

The Windsoar was planned to be delivered to buyers as an assembly kit that would take about 100–200 hours to complete. The major structural assembly would be completed at the factory and the builder would have been required to complete the bolting and riveting, as well as installing the fabric.[1]

Project 102 was supposed to fly in the summer of 1982, with kit production commencing the following autumn and winter and customer deliveries in the spring of 1983.[1] The aircraft never entered production.

Specifications (Project 102)

{{Aircraft specs
|ref=
|prime units?=imp


|genhide=
|crew=one
|capacity=
|length m=
|length ft=19
|length in=6
|length note=
|span m=
|span ft=37
|span in=6
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=200
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=1
|eng1 name=two stroke
|eng1 type=
|eng1 kw=
|eng1 hp=10
|eng1 kn=
|eng1 lbf=
|eng1 note= to 25 hp (19 kW)
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=
|max speed mph=90
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=20
|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=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=+6/-6
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2
|disk loading lb/sqft=
|disk loading note=
|more performance=


|armament=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

{{commons category|Birdman Enterprises}}
1. ^Taylor, John WR: Janes All the Worlds Aircraft 1982-83 page 626, Janes Publishing Company, 1982. {{ISBN|0-7106-0748-2}}
{{Birdman Enterprises}}

2 : Canadian sailplanes 1980–1989|Canadian experimental 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:2024/9/20 9:41:16