请输入您要查询的百科知识:

 

词条 Softeks V-24 Lastivka
释义

  1. Design and development

  2. Specifications (Rotax 912 ULS)

  3. References

name=V-24 Lastivka image= caption=

}}{{Infobox Aircraft Type

type=Four seat twin engined pusher utility aircraft national origin=Ukraine manufacturer=Softeks designer=Victor Vashchenko first flight=20 November 2012 introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost=Target price $420,000 developed from= variants with their own articles=
}}

The Softeks V-24 Lastivka (Ластівка, Swallow) is a four seat, twin pusher engined utility aircraft, designed and built in Ukraine in the 2010s for survey and transport work. The first prototype flew late in 2012.

Design and development

The Lastochka is designed for a wide range of utility work, such as fire and geological surveys, freight transport and passenger carrying. It is a low wing monoplane constructed largely of composites, with straight tapered wings tipped with winglets. Their trailing edges carry slotted ailerons and slotted flaps. Two {{convert|73.5|kW|hp|abbr=on|0}} Rotax 912 ULS air-cooled flat four engines are mounted in pusher configuration on pylons over the wings in short cowlings, positioned with their propeller discs as close as possible to the fuselage. {{convert|84.5|kW|hp|abbr=on|0}} Rotax 914 engines are an alternative.

The nose and cabin transparencies are smoothly contoured, with no windscreen step, and entry is by an upward opening door on each side forward of the wing leading edge. There are transparencies aft of those in the doors, placed over the wing. A baggage space has a maximum volume of 0.20 m3 (7.0 cu ft), depending on layout details. The upper fuselage line drops gently behind the cabin to the T-tail, where the fin is integral with the fuselage, straight edged and swept, with a backward leaning rudder hinge. The rudder, with a swept trailing edge, has a horn balance extending forward of the hinge line under the fuselage, where it is faired into a small ventral fin. There is a small, electrically activated rudder trim tab, set low down. A high aspect ratio, rectangular tailplane is placed on top of the fin, bearing a similarly shaped one piece elevator. This has a central trim tab.

The Lastochka has a tricycle undercarriage with main legs retracting inwards; each leg has a pneumatic shock absorber and carries a single wheel fitted with hydraulic brakes. The nosewheel retracts forwards. The aircraft is designed to operate from water or snow, using floats or skis, if required.

The first flight took place on 20 November 2012 and the Lastochka was first demonstrated in public at the SP Korolyov Aviation Meeting, held from 17-20 Jane 2010 at Smokovka airport, Zhytomyr.

Specifications (Rotax 912 ULS)

{{Aircraft specs
|ref=Jane's All the World's Aircraft 2013-14, pp.655-6
|prime units?=met


|genhide=
|capacity=Four, including one or two pilots
|length m=7.34
|length note=
|span m=11.18
|span note=
|height m=2.98
|wing area sqm=11.74
|wing area note=gross
|aspect ratio=
|airfoil=
|empty weight kg=760
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1300
|max takeoff weight note=
|fuel capacity=250 L (55 Imp gal; 66 US gal); 180 kg (396 lb). Provision for additional tankage.
|more general=

  • Maximum payload: 400 kg (881 kg)
  • Take-off run: 250 m (821 ft)
  • Landing run: 200 m (656 ft)
  • Recovery parachute: Galaxy GRS 1200 ballistic


|eng1 number=2
|eng1 name=Rotax 912 ULS
|eng1 type=liquid cooled flat four
|eng1 kw=73.5
|eng1 hp=
|eng1 note=
|power original=
|thrust original=
|more power=
|prop blade number=2
|prop name=MT-Propeller MTV-21-A-C-F/CFL0178-51
|prop dia m=1.78
|prop dia note= variable pitch pusher


|perfhide=
|max speed kmh=300
|max speed note=
|cruise speed kmh=265
|cruise speed note=at 65% power
|stall speed kmh=90
|stall speed note=flaps down
|never exceed speed kmh=350
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=1500
|range note=
|endurance=
|ceiling m=5100
|ceiling note=service
|g limits=
|roll rate=
|climb rate ms=8.0
|climb rate note=at sea level
|time to altitude=
|lift to drag=
|wing loading kg/m2=110.7
|wing loading note=maximum
|power/mass=113 W/kg (0.069 hp/lb) minimum
|more performance=
|avionics=

  • Dynon Avionics twin screen electronic flight instrument system
  • Autopilot

}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References


}}

4 : Ukrainian civil utility aircraft 2010–2019|Low-wing aircraft|Twin-engined pusher aircraft|Aircraft first flown in 2012

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:2024/9/21 16:46:48