请输入您要查询的百科知识:

 

词条 Golden Gate Mosquito
释义

  1. Design and development

  2. Specifications (Mosquito)

  3. See also

  4. References

name=Mosquito image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft national origin=United States manufacturer=Golden Gate Aviation designer= first flight= introduced= retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= developed from= Phantom X1 variants with their own articles=
}}

The Golden Gate Mosquito is an American ultralight aircraft that was produced by Golden Gate Aviation. The aircraft was supplied as a kit for amateur construction.[1]

Design and development

A copy of the popular Phantom X1, the Mosquito 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|252|lb|kg|0|abbr=on}}. It features a strut-braced or optionally cable-braced high-wing, a single-seat, open cockpit, tricycle landing gear and a single engine in tractor configuration.[1]

The aircraft is made from aluminum tubing, with the flying surfaces covered in Dacron sailcloth. Its {{convert|29|ft|m|1|abbr=on}} span wing was available in a strut-braced or cable-braced configuration, the cable bracing giving better negative g performance. On the cable-braced version the ground wires are supported by an inverted "V" kingpost. The aircraft is rated for load limits of +10/-6 g. The pilot is accommodated on a seat within a semi-enclosed fiberglass pod that includes a windshield. The standard engine is a Kawasaki 440 snowmobile engine of {{convert|35|hp|kW|0|abbr=on}}, mounted at the front of the main fuselage keel tube, above the pilot. The cruciform tail is mounted at the aft end of the same keel tube.[1]

Specifications (Mosquito)

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


|genhide=
|crew=one
|capacity=
|length m=
|length ft=15.1
|length in=
|length note=
|span m=
|span ft=29
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=145
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=252
|empty weight note=
|gross weight kg=
|gross weight lb=502
|gross weight note=
|fuel capacity={{convert|5|u.s.gal}}
|more general=


|eng1 number=1
|eng1 name=Kawasaki 440
|eng1 type=twin cylinder, two-stroke snowmobile engine
|eng1 kw=
|eng1 hp=35
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=63
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=60
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=26
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=100
|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=+10/-6
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=790
|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=3.46
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

See also

{{aircontent
|see also=
|related=
  • Phantom X1

|similar aircraft=
|lists=
}}

References

1. ^Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-27. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}

3 : United States ultralight aircraft 1980–1989|Homebuilt aircraft|Single-engined tractor 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:2024/11/13 20:31:05