请输入您要查询的百科知识：

　

词条 Millennium Master
释义

  1. Design and development

  2. Specifications (912 ULS engine)

  3. References

name=Master image= caption=

}}{{Infobox Aircraft Type

 type=Tandem seat ultralight national origin=Italy manufacturer=Millennium Aircraft (Compact Compositi srl), Turin designer= first flight=27 May 2006 introduced= retired= status= primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=Blackshape Prime
Pelegrin Tarragon
}}

The Millennium Master is a low wing, single engine, tandem two-seat ultralight aircraft, constructed chiefly of carbon fibre. Designed and built in Italy, it flew for the first time in 2006.

Design and development

The design of the Millennium Master stemmed from that of an earlier, wooden Asso X kit built aircraft but the structure has been entirely transformed into prepreg carbon fibre by Millennium Aircraft. The structural design was done by the Department of Aerostructures at the University of Turin and the aerodynamics were investigated by Alenia.

The Master has a low set, trapezoidal wing, though that plan is modified by an extended wing root fairing or glove, plus wing tips of the Küchemann type with curved leading edges. Flaps occupy the whole trailing edge inboard of the ailerons and have four settings. These flaps are slotted and are each in two spanwise parts, the break placed at the wing fold hinge line.

A single piece canopy covers the tandem seats, with the rear seat higher than the other. Behind the cockpit the fuselage line falls to the tail. The tailplane is straight edged with rounded tips and carries marked anhedral. The fin and rudder are also straight edged but swept; there is a small additional ventral fin. Elevator has trim tabs. The Master has a tricycle undercarriage, the nosewheel retracting rearwards and the main legs inwards into the wings. The track is 2.01 m (6 ft 7 in).

The Master is powered by a Rotax 912 ULS 100 HP (74 kW). It drives a two blade propeller with variable pitch in flight.

The Master first flew on 27 May 2006 and appeared in public for the first time at Aero '07 at Friedrichshafen in Germany in 2007. A second prototype flew in December 2007. Production was planned to start in October 2007, beginning with complete aircraft before commencing kit production.

The company went bankrupt before production of the Master was started and the design was later acquired by Blackshape of Monopoli, Italy and developed into the Blackshape Prime. The design was also developed into the Pelegrin Tarragon by Pelegrin Limited in conjunction with CFM Air.[1][2]

Specifications (912 ULS engine)

{{Aircraft specs
|ref=Jane's All the World's Aircraft 2010/11
|prime units?=met


|genhide=
|crew=
|capacity=2
|length m=7.18
|length ft=
|length in=
|length note=
|span m=7.94
|span ft=
|span in=
|span note=
|height m=2.41
|height ft=
|height in=
|height note=
|wing area sqm=9.96
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=285
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=450
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=4-cylinder horizontally opposed
|eng1 kw=59.6
|eng1 hp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|more power=
|prop blade number=2
|prop name=with ground-adjustable pitch
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=306
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=62
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=378
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|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=
|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
|wing loading lb/sqft=
|wing 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=
}}

References

1. ^Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 33. WDLA UK, Lancaster UK, 2011. {{ISSN|1368-485X}}
2. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 72. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

}}

3 : Italian sport aircraft 2000–2009|Low-wing aircraft|Aircraft first flown in 2006
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 9:35:38