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词条 Fly Castelluccio Mach
释义

  1. Design and development

  2. Variants

  3. Specifications (Mach 1)

  4. References

  5. External links

name= Mach image= caption=

}}{{Infobox Aircraft Type

 type=Paramotor national origin=Italy manufacturer=Fly Castelluccio designer= first flight=2000s introduced= retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= €2,944 (March 1, 2004) developed from= variants with their own articles=
}}

The Fly Castelluccio Mach is a family of Italian paramotors that was designed and produced by Fly Castelluccio of Ascoli Piceno for powered paragliding. Now out of production, when it was available the aircraft were supplied complete and ready-to-fly.[1]

Design and development

The Mach was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration powering a two-bladed or four-bladed wooden propeller through a reduction drive.[1]

As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]

Variants

Mach 1 Light

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|122|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|10|l}}, with an additional {{convert|5|l}} optional.[1][2]

Mach 2

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|68|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|8.5|l}}.[1][3]

Mach 2 4BL

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|80|cm|in|0|abbr=on}} diameter four-bladed wooden propeller. The fuel tank capacity is {{convert|8.5|l}}, with an additional {{convert|5|l}} optional.[3]

Mach 3

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|94|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|8.5|l}}, with an additional {{convert|5|l}} optional.[1][4]

Mach 3 4BL

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|94|cm|in|0|abbr=on}} diameter four-bladed wooden propeller. The fuel tank capacity is {{convert|8.5|l}}, with an additional {{convert|5|l}} optional.[4]

Mach 4

Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a reduction drive and a {{convert|114|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|10|l}}, with an additional {{convert|5|l}} optional.[1][5]

Mach 4C

Model optimized for endurance competition flying, with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 EVO engine in pusher configuration with a reduction drive and a {{convert|114|to|130|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|10|l}}, with an additional {{convert|5|l}} optional.[5]

Specifications (Mach 1)

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


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=18
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|10|l}}, with an additional {{convert|5|l}} optional for a total of {{convert|15|l}}
|more general=


|eng1 number=1
|eng1 name=Solo 210
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a reduction drive
|eng1 kw=
|eng1 hp=14
|prop blade number=2
|prop name=wooden, fixed pitch
|prop dia m=1.22
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=Y
|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=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^1 2 3 4 5 6 7 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 67. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
2. ^{{cite web|url=http://www.flycastelluccio.it/paramotor/paramotor_mach1.asp|archiveurl=https://web.archive.org/web/20040401102724/http://www.flycastelluccio.it/paramotor/paramotor_mach1.asp|title=Mach 1 Paramotor|archivedate=1 April 2004|author=Fly Castelluccio|work=flycastelluccio.it|accessdate=25 October 2015}}
3. ^1 {{cite web|url=http://www.flycastelluccio.it/paramotor/paramotor_mach2.asp|archiveurl=https://web.archive.org/web/20040204065743/http://www.flycastelluccio.it/paramotor/paramotor_mach2.asp|title=Mach 2 Paramotor|author=Fly Castelluccio|archivedate=4 February 2004|work=flycastelluccio.it|accessdate=25 October 2015}}
4. ^1 {{cite web|url=http://www.flycastelluccio.it/paramotor/paramotor_mach3.asp|archiveurl=https://web.archive.org/web/20040401105557/http://www.flycastelluccio.it/paramotor/paramotor_mach3.asp|title=Mach 3 Paramotor|author=Fly Castelluccio|archivedate=1 April 2004|work=flycastelluccio.it|accessdate=25 October 2015}}
5. ^1 {{cite web|url=http://www.flycastelluccio.it/paramotor/paramotor_mach3.asp|archiveurl=https://web.archive.org/web/20040204011454/http://www.flycastelluccio.it/paramotor/paramotor_mach4.asp|title=Mach 4 Paramotor|author=Fly Castelluccio|archivedate=1 April 2004|work=flycastelluccio.it|accessdate=25 October 2015}}

External links

  • {{Official website|https://web.archive.org/web/20040401102724/http://www.flycastelluccio.it/paramotor/paramotor_mach1.asp}} archive
{{Fly Castelluccio aircraft}}

4 : Fly Castelluccio aircraft|Italian ultralight aircraft 2000–2009|Single-engined pusher aircraft|Paramotors
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