Nova Radon

{|{{Infobox Aircraft Begin
| name= Radon
| image=
| caption=
}}{{Infobox Aircraft Type
| type=[[Paraglider]]
| national origin=[[Austria]]
| manufacturer=[[Nova Performance Paragliders]]
| designer=Hannes Papesch
| first flight=
| introduced=
| retired=
| status=Production completed
| primary user=
| more users= <!--Limited to three in total; separate using <br /> -->
| produced= <!--years in production-->
| number built=
| program cost= <!--Total program cost-->
| unit cost= [[Pound sterling|£]]1,914 (2004)
| developed from=
| variants with their own articles=
}}
|}
The '''Nova Radon''' is an [[Austria]]n single-place [[paraglider]] that was designed by Hannes Papesch and produced by [[Nova Performance Paragliders]] of [[Innsbruck]]. It is now out of production.<ref name="WDLA04">Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003–04'', page 23. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}</ref>

==Design and development==
The aircraft was designed as an advanced performance glider. The models are each named for their relative size.<ref name="WDLA04"/>
<!-- ==Operational history== -->

==Variants==
;Radon XS
:Extra small-sized model for lighter pilots. Its {{convert|11.35|m|ft|1|abbr=on}} span wing has a wing area of {{convert|20.18|m2|sqft|abbr=on}}, 57 cells and the [[Aspect ratio (aeronautics)|aspect ratio]] is 5.66:1. The pilot weight range is {{convert|60|to|85|kg|lb|0|abbr=on}}. The glider model is IA certified.<ref name="WDLA04"/>
;Radon S
:Small-sized model for light pilots. Its {{convert|11.9|m|ft|1|abbr=on}} span wing has a wing area of {{convert|22.17|m2|sqft|abbr=on}}, 57 cells and the aspect ratio is 5.66:1. The pilot weight range is {{convert|75|to|95|kg|lb|0|abbr=on}}. The glider model is DHV 2 and AFNOR Performance certified.<ref name="WDLA04"/>
;Radon M
:Mid-sized model for medium-weight pilots. Its {{convert|12.42|m|ft|1|abbr=on}} span wing has a wing area of {{convert|24.16|m2|sqft|abbr=on}}, 57 cells and the aspect ratio is 5.66:1. The pilot weight range is {{convert|90|to|110|kg|lb|0|abbr=on}}. The glider model is DHV 2 and AFNOR Performance certified.<ref name="WDLA04"/>
;Radon L
:Large-sized model for heavier pilots. Its {{convert|12.91|m|ft|1|abbr=on}} span wing has a wing area of {{convert|26.13|m2|sqft|abbr=on}}, 57 cells and the aspect ratio is 5.66:1. The pilot weight range is {{convert|95|to|130|kg|lb|0|abbr=on}}. The glider model is DHV 2 and AFNOR Performance certified.<ref name="WDLA04"/>
<!-- ==Aircraft on display== -->

==Specifications (Radon M) ==
{{Aircraft specs
|ref=Bertrand<ref name="WDLA04" />
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
General characteristics
-->
|genhide=

|crew=one
|capacity=
|length m=
|length ft=
|length in=
|length note=
|span m=12.42
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=24.16
|wing area sqft=
|wing area note=
|aspect ratio=5.66:1
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|more general=
<!--
Performance
-->
|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=
|g limits=
|roll rate=
|glide ratio=<!-- at {{convert|XX|km/h|mph|0|abbr=on}} -->
|sink rate ms=
|sink rate ftmin=
|sink rate note=<!-- at {{convert|XX|km/h|mph|0|abbr=on}} -->
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
}}

==References==
{{reflist}}

<!-- ==External links== -->
{{Nova aircraft}}
[[Category:Nova aircraft|Radon]]
[[Category:Paragliders]]