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词条 Aero Nord AIR
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Specifications (AIR 1)

  5. References

name= AIR image= caption=

}}{{Infobox Aircraft Type

type=Paramotor national origin=France manufacturer=Aero Nord ULM designer= first flight= introduced= retired= status=Production completed primary user= more users= produced= number built= program cost= unit cost= €2,900 (AIR 1, 2004) developed from= variants with their own articles=
}}

The Aero Nord AIR series is a family of French paramotors that was designed and produced by Aero Nord of Lorgies, and later Bénifontaine, for powered paragliding. Now out of production, when it was available the aircraft was supplied as a complete and ready-to-fly.[1]

Design and development

The aircraft 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|22|hp|kW|0|abbr=on}} RDM engine in pusher configuration with a 4:1 ratio reduction drive and a {{convert|100|to|125|cm|in|0|abbr=on}} diameter two-bladed wooden propeller. The fuel tank capacity is {{convert|9|l}}. As is the case with all paramotors, take-off and landing is accomplished by foot.[1]

The aircraft is built with a welded aluminium tubing propeller cage, which can be broken down into two or four sections for ground stowage. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]

Operational history

Reviewer Rene Coulon wrote in 2003 that the "machine shows good understanding of the market and skill in the production" and noted that the series has attracted "considerable attention".[1]

Variants

AIR 1

Single place paramotor, with an empty weight of {{convert|21|kg|lb|0|abbr=on}} and a single {{convert|22|hp|kW|0|abbr=on}} RDM engine with a {{convert|100|cm|in|0|abbr=on}} diameter two-bladed wooden propeller.[1]

AIR 2

Single place paramotor, with an empty weight of {{convert|21.5|kg|lb|0|abbr=on}} and a single {{convert|22|hp|kW|0|abbr=on}} RDM engine with a {{convert|113|cm|in|0|abbr=on}} diameter two-bladed wooden propeller.[1]

AIR 3

Single place paramotor, with an empty weight of {{convert|21.5|kg|lb|0|abbr=on}} and a single {{convert|22|hp|kW|0|abbr=on}} RDM engine with a {{convert|125|cm|in|0|abbr=on}} diameter two-bladed wooden propeller.[1]

Specifications (AIR 1)

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


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
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|span m=
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|wing area sqm=
|wing area sqft=
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|aspect ratio=
|airfoil=
|empty weight kg=21
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|9|l}}
|more general=


|eng1 number=1
|eng1 name=RDM
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a 4:1 reduction drive
|eng1 kw=
|eng1 hp=22
|prop blade number=
|prop name=
|prop dia m=
|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. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 62. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X

4 : Aero Nord aircraft|French ultralight aircraft 2000–2009|Single-engined pusher aircraft|Paramotors

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