请输入您要查询的百科知识:

 

词条 Hoffmann H40
释义

  1. Specifications

  2. References

name=H40image=caption=

}}{{Infobox Aircraft Type

type=Sport aircraftnational origin=Germanymanufacturer=Hoffmanndesigner=Wolf Hoffmann1988}}introduced=retired=status=primary user=more users=produced=number built=1variants with their own articles=
}}

The Hoffmann H40 was a prototype sport aircraft built in Germany in 1988. Designed by Wolf Hoffmann based on his Dimona motor-glider, it was a conventional, low-wing monoplane with side-by-side seating for two and tricycle undercarriage. The aircraft's high aspect ratio wings and T-tail were carried over from its motorglider heritage, but the span was shorter than that of the Dimona. Construction throughout was of composite materials. Hoffmann intended this aircraft to compete with sporting two-seaters such as the Grob G 115 and Robin ATL, but was unable to find the financial backing to bring the aircraft to market, despite a 30% share bought in the project by German pump manufacturer ABS.

Specifications

{{aerospecs
|ref=Jane's All The World's Aircraft 1988-89[1]
|met or eng?=met
|crew=One pilot
|capacity=1 passenger
|length m=7.26
|length ft=24
|length in=11¾
|span m=10.76
|span ft=35
|span in=3½
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=2.39
|height ft=7
|height in=10
|wing area sqm=13.62
|wing area sqft=145.3
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=590
|empty weight lb=1,300
|gross weight kg=850
|gross weight lb=1,874
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Lycoming O-235 flat-four
|eng1 kw=86.5
|eng1 hp=116
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|perfhide=
|max speed kmh=210
|max speed mph=130
|max speed mach=
|cruise speed kmh=180
|cruise speed mph=111[2]
|range km=680
|range miles=422
|endurance h=
|endurance min=
|ceiling m=4,500
|ceiling ft=14,800
|glide ratio=
|climb rate ms=3.6
|climb rate ftmin=700
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

1. ^Lambert 1993, p.104.
2. ^econ cruise
  • {{cite book|last=Lambert |first=Mark |title=Jane's All the World's Aircraft 1993-94|year=1993 |publisher=Jane's Data Division |location=Coulsdon, UK|isbn=0-7106-1066-1 }}
  • {{cite book|last=Taylor |first=John W.R. |title=Jane's All the World's Aircraft 1987-88|year=1987 |publisher=Jane's Yearbook |location=London |page=98|isbn=0-7106-0850-0 }}
  • {{cite book |last=Taylor |first=John W.R. |title=Jane's All The World's Aircraft 1988-89 |year= 1988|publisher=Jane's Defence Data |location=Couldon, UK |isbn=0-7106-0867-5 |page= |pages= |url= |accessdate=}}
  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |page=929 |isbn= 0-7106-0710-5 }}
  • {{cite book |last= Simpson |first= R. W. |title=Airlife's General Aviation |year=1995 |publisher=Airlife Publishing |location=Shrewsbury |pages=214 |isbn= 1-85310-577-5 }}
  • {{cite journal |title=Hoffmann Seeks Producer |journal=Flight International |date=27 June 1987 |pages=63–64 |url=http://www.flightglobal.com/pdfarchive/view/1987/1987%20-%200953.html |accessdate=2008-05-04}}
  • {{cite journal |title=Hoffmann finds backer for light trainer |journal=Flight International |date=27 February 1988 |pages=15 |url=http://www.flightglobal.com/pdfarchive/view/1988/1988%20-%200467.html |accessdate=2008-05-04}}
{{Hoffmann aircraft}}

5 : German sport aircraft 1980–1989|Hoffmann aircraft|Low-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1988

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:2024/11/10 17:41:29