请输入您要查询的百科知识:

 

词条 Jastreb Vuk-T
释义

  1. Design and development

  2. Specifications (Vuk-T)

  3. Notes

  4. References

  5. External links

name=Vuk-T image=Vuk T glider on apron of AKNM after a local soaring flight.jpg caption=

}}{{Infobox Aircraft Type

type=Standard Class Sailplane national origin=Yugoslavia manufacturer=FAJ Jastreb designer=Prof. Dr. Tomislav Dragović first flight= introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The FAJ Jastreb Vuk-T often called Vuk (Serbian:Vuk - Wolf) is a Standard Class single-seat high-performance glider, intended for transition training, designed and built in the Yugoslavia from the late 1970s.

Design and development

Designed by Prof. Dr. Tomislav Dragović at the Faculty of Mechanical Engineering, Aero Engineering Institute, University of Belgrade, the Vuk-T was manufactured by FAJ Jastreb in Vršac entirely from fiberglass. After manufacture the gliders were first tested by the JRV and JNA before donation to state-sponsored aero clubs across the country.

Permitted to do the following aerobatic manoeuvres: loop, stall turn, steep turn and spin, the Vuk-t is popular in flying clubs because it reminds club members about free flying, the free donation of planes to clubs by the army and general Yugoslavian nostalgia. The majority of surviving Vuk-t gliders fly with aero-clubs with few aircraft in private ownership and are expected to have a long life due to the high structural strength and ease of maintenance.

One peculiar attribute of the VUK-T can be characterized by a whistling sound when flying, often described as the howl of a wolf, (vuk meaningwolf in some languages used by peoples of the former Yugoslavia.

Specifications (Vuk-T)

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


|genhide=
|crew=1
|capacity=
|length m=6.5
|length ft=
|length in=
|length note=
|span m=15
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=1.3
|height ft=
|height in=
|height note=
|wing area sqm=11.955
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil= NASA GA(W)-1
|empty weight kg=260
|empty weight lb=
|empty weight note=
|gross weight kg=385
|gross weight lb=
|gross weight note=

  • Minimum pilot weight equipped: {{convert|70|kg|lb|abbr=on|0}}
  • Maximum pilot weight equipped: {{convert|110|kg|lb|abbr=on|0}}

|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=59
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=240
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=

  • Max Rough air speed {{convert|150|km/h|kn mph|abbr=on|0}}
  • Max Aerotow speed {{convert|125|km/h|kn mph|abbr=on|0}}
  • Max Winch launch speed {{convert|110|km/h|kn mph|abbr=on|0}}

|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=
|roll rate=
|glide ratio=37.5 at {{convert|105|km/h|kn mph|abbr=on|0}}
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=0.65
|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=
|power/mass=
|thrust/weight=
|more performance=


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

  • List of gliders

}}

Notes

1. ^{{cite web|title=Our gliders FAJ Jastreb Vršac Yugoslavia|url=http://airserbia.com/fetch_file.php?id=79&action=download|publisher=FAJ Jastreb|language=Serbian|accessdate=18 January 2013}}

References

{{refbegin}}
  • {{cite web|title=Our gliders FAJ Jastreb Vršac Yugoslavia|url=http://airserbia.com/fetch_file.php?id=79&action=download|publisher=FAJ Jastreb|language=Serbian|accessdate=18 January 2013}}
{{refend}}

External links

  • Vuk-T Handbook (in Serbian)
{{DEFAULTSORT:Vuk-T (Glider)}}

2 : Glider aircraft|Yugoslav sailplanes 1970–1979

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:2024/9/23 10:20:34