请输入您要查询的百科知识:

 

词条 Aeros del Sur Manta
释义

  1. Design and development

  2. Specifications (Manta)

  3. References

  4. External links

name=Manta image= caption=

}}{{Infobox Aircraft Type

type=Ultralight trike national origin=Argentina manufacturer=Aeros del Sur designer= first flight= introduced= retired= status=In production (2013) primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Aeros del Sur Manta is an Argentine ultralight trike, designed and produced by Aeros del Sur. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Design and development

Aeros del Sur is the importer of Aeros products for Argentina. The Manta was designed by mating the Aeros Profi trike wing with a new, locally designed carriage. The Manta was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of {{convert|472.5|kg|lb|0|abbr=on}}, with a ballistic parachute. The Manta has a maximum gross weight of {{convert|472.5|kg|lb|0|abbr=on}}. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.[1]

The aircraft is made from a mix of bolted-together aluminum and steel tubing, with its double surface wing covered in Dacron sailcloth. Its {{convert|10|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The standard powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine, but the HKS 700E four-stroke, dual-ignition {{convert|60|hp|kW|0|abbr=on}} engine is optional, as are Hirth and Simonini powerplants.[1]

Specifications (Manta)

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


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=10
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=15.4
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|50|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 582
|eng1 type=two cylinder, liquid-cooled, two stroke aircraft engine
|eng1 kw=48
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|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=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=30.68
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 198. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

External links

  • {{Official website|https://web.archive.org/web/20130522032529/http://aerosdelsur.com.ar/}}

3 : Argentine ultralight aircraft 2000–2009|Single-engined pusher aircraft|Ultralight trikes

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 18:02:32