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词条 Gradient Avax
释义

  1. Design and development

  2. Variants

  3. Specifications (Avax RSE 26)

  4. References

  5. External links

name=Avax image=File:GradientAvaxXC.jpg caption=Avax XC

}}{{Infobox Aircraft Type

type=Paraglider national origin=Czech Republic manufacturer=Gradient sro designer= first flight= introduced= retired= status=In production (2016) primary user= more users= produced= program cost= unit cost= €2,884 (Avax RSE 26, 2004) developed from= variants with their own articles=
}}

The Gradient Avax is a Czech single-place, paraglider designed and produced by Gradient sro of Prague. Introduced in the early 2000s, it remained in production in 2016 as the Avax XC5.[1]

Design and development

The Avax was designed as a competition glider.[1]

The design has progressed through five generations of models, the Avax, Avax 2, 3, 4 and 5, each improving on the last. The models are each named for their approximate wing area in square metres.[1]

The Avax XC5 employs a unit cell structure that uses a combination of two non-carrying ribs with double diagonal segmented ribs attached to the wing's top surface. The wing trailing edge employs mini-ribs to maintain a smooth profile.[2]

Variants

Avax RSE 24

Small-sized model for lighter pilots. Its {{convert|11.97|m|ft|1|abbr=on}} span wing has a wing area of {{convert|22.62|m2|sqft|abbr=on}}, 73 cells and the aspect ratio is 6.38:1. The pilot weight range is {{convert|70|to|85|kg|lb|0|abbr=on}}.[1]

Avax RSE 26

Mid-sized model for medium-weight pilots. Its {{convert|12.67|m|ft|1|abbr=on}} span wing has a wing area of {{convert|25.17|m2|sqft|abbr=on}}, 73 cells and the aspect ratio is 6.38:1. The pilot weight range is {{convert|85|to|105|kg|lb|0|abbr=on}}. The glider model is AFNOR Competition certified.[1]

Avax RSE 28

Large-sized model for heavier pilots. Its {{convert|13.20|m|ft|1|abbr=on}} span wing has a wing area of {{convert|27.31|m2|sqft|abbr=on}}, 73 cells and the aspect ratio is 6.38:1. The pilot weight range is {{convert|95|to|120|kg|lb|0|abbr=on}}.[1]

Avax XC5 24

Small-sized model for lighter pilots. Its {{convert|12.2|m|ft|1|abbr=on}} span wing has a wing area of {{convert|21.4|m2|sqft|abbr=on}}, 66 cells and the aspect ratio is 6.96:1. The takeoff weight range is {{convert|70|to|85|kg|lb|0|abbr=on}}. The glider model is EN/LTF-D certified.[3]

Avax XC5 26

Mid-sized model for medium-weight pilots. Its {{convert|12.79|m|ft|1|abbr=on}} span wing has a wing area of {{convert|23.5|m2|sqft|abbr=on}}, 66 cells and the aspect ratio is 6.96:1. The takeoff weight range is {{convert|82|to|97|kg|lb|0|abbr=on}}. The glider model is EN/LTF-D certified.[3]

Avax XC5 28

Large-sized model for heavier pilots. Its {{convert|13.38|m|ft|1|abbr=on}} span wing has a wing area of {{convert|25.7|m2|sqft|abbr=on}}, 66 cells and the aspect ratio is 6.96:1. The takeoff weight range is {{convert|95|to|118|kg|lb|0|abbr=on}}. The glider model is EN/LTF-D certified.[3]

Specifications (Avax RSE 26)

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


|genhide=
|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=12.67
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=25.17
|wing area sqft=
|wing area note=
|aspect ratio=6.38:1
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|more general=


|perfhide=
|max speed kmh=60
|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=
|g limits=
|roll rate=
|glide ratio=
|sink rate ms=1.0
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
}}

References

1. ^Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 19. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X
2. ^{{cite web|url = http://www.gradient.cx/en/AvaxXC5|title = Avax XC5|accessdate = 29 May 2016|author = Gradient sro|date = }}
3. ^{{cite web|url=http://www.gradient.cx/en/AvaxXC5/tech |title=Avax XC5 Technical Data |accessdate=29 May 2016 |author=Gradient sro |date= |deadurl=yes |archiveurl=https://web.archive.org/web/20160625041842/http://www.gradient.cx/en/AvaxXC5/tech |archivedate=25 June 2016 |df= }}

External links

{{Commons category|Gradient Avax}}
  • {{Official website|http://www.gradient.cx/en/AvaxXC5}}
{{Gradient aircraft}}

2 : Gradient aircraft|Paragliders

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