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词条 P&M PulsR
释义

  1. Design and development

  2. Operational history

  3. Specifications (PulsR)

  4. References

  5. External links

{{Use dmy dates|date=February 2018}}{{Use British English|date=February 2018}}
name= PulsR image=File:P & M Aviation PulsR G-SFCM (41182560425).jpg caption=

}}{{Infobox Aircraft Type

type=Ultralight trike national origin=United Kingdom manufacturer=P&M Aviation designer=Bill Brooks first flight= introduced=2011 retired= status=In production (2018) primary user= more users= produced= 2015-present number built= program cost= unit cost= €45,260 (2015) developed from= variants with their own articles=
}}

The P&M PulsR ({{lang-en|Pulsar}}) is a British ultralight trike, designed by Bill Brooks and produced by P&M Aviation of Rochdale. The aircraft is supplied complete and ready-to-fly.[1]

The design was introduced publicly at the Flying Show in Birmingham in December 2011, where writer Demitri Delemarle reported that it "stole the show", due to its unusual semi-enclosed cockpit design.[1]

Design and development

The PulsR 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 aircraft has a maximum gross weight of {{convert|472.5|kg|lb|0|abbr=on}} with a ballistic parachute and {{convert|450|kg|lb|0|abbr=on}} without.[1]

The design was first shown in 2011 and remained in prototype-only form until 2015.[1]

The aircraft design features a strut-braced topless hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem semi-enclosed cockpit with a cockpit fairing and windshield, tricycle landing gear with main gear wheel pants and a single engine in pusher configuration.[1]

The aircraft fuselage is a monocoque design made from composite carbon fibre, with its double surface wing covered in Dacron sailcloth. Its {{convert|9.26|m|ft|1|abbr=on}} span wing is supported by struts and uses an "A" frame weight-shift control bar, which is routed though the open side window spaces in the semi-enclosed fairing. The powerplant is a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS engine.[1][2]

The aircraft has an empty weight of {{convert|251|kg|lb|0|abbr=on}} and a gross weight of {{convert|472.5|kg|lb|0|abbr=on}}, giving a useful load of {{convert|222|kg|lb|0|abbr=on}}. With full fuel of {{convert|78|l}} the payload is {{convert|166|kg|lb|0|abbr=on}}.[1][2]

Operational history

Writer Demitri Delemarle reports that the design "never fails to attract attention" wherever it is shown, due to its unusual aerodynamic cockpit design, which makes it much faster and gives a better glide ratio than other trikes.[1]

Specifications (PulsR)

{{Aircraft specs
|ref=Tacke and manufacturer[1][2]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=3.2
|length ft=
|length in=
|length note=
|span m=9.26
|span ft=
|span in=
|span note=
|height m=2.82
|height ft=
|height in=
|height note=
|wing area sqm=13
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=251
|empty weight lb=
|empty weight note=with ballistic parachute fitted
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|78|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=75
|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=105
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=95
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=39
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=120
|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=+6g/-3g (ultimate)
|roll rate=
|glide ratio=12:1
|climb rate ms=
|climb rate ftmin=1000
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=410
|sink rate note=
|lift to drag=
|wing loading kg/m2=36.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 236. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^{{cite web|url =http://www.pmaviation.co.uk/pulsr-ouraircraftdetails.html|title = PulsR|accessdate = 28 February 2018|author=P&M Aviation |work =www.pmaviation.co.uk |year=2014}}

External links

  • {{Official website|http://www.pmaviation.co.uk/pulsr-ouraircraftdetails.html}}
{{P&M Aviation aircraft}}{{DEFAULTSORT:PandM PulsR}}

5 : P&M Aviation aircraft|British sport aircraft 2010–2019|British ultralight aircraft 2010–2019|Single-engined pusher aircraft|Ultralight trikes

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