Zero Gravity Flow

{|{{Infobox Aircraft Begin
| name= Flow
| image=
| caption=
}}{{Infobox Aircraft Type
| type=[[Paraglider]]
| national origin=[[South Korea]]
| manufacturer=[[Zero Gravity Paragliders]]
| designer=Mansoo Chae
| first flight=
| introduced=2002
| retired=
| status=Production completed
| primary user=
| more users= <!--Limited to three in total; separate using <br /> -->
| produced= mid-2000s
| number built=
| program cost= <!--Total program cost-->
| unit cost=
| developed from=
| variants with their own articles=
}}
|}
The '''Zero Gravity Flow''' is a [[South Korea]]n single-place [[paraglider]] that was designed by Mansoo Chae and produced by [[Zero Gravity Paragliders]] of [[Seoul]], introduced in 2002. It is now out of production.<ref name="WDLA04">Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 38. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}</ref>

==Design and development==
The Flow was designed as a beginner glider for [[flight training]]. The models are each named for their relative size.<ref name="WDLA04"/>

By 2003 glider was initially to be only sold in South Korea, with global marketing to follow.<ref name="WDLA04"/>
<!-- ==Operational history== -->

==Variants==
;Flow XS
:Extra small-sized model for lighter pilots. Its {{convert|10.6|m|ft|1|abbr=on}} span wing has a wing area of {{convert|24.1|m2|sqft|abbr=on}}, 35 cells and the [[Aspect ratio (aeronautics)|aspect ratio]] is 4.7:1. The pilot weight range is {{convert|60|to|80|kg|lb|0|abbr=on}}. In 2003 the glider model was undergoing certification.<ref name="WDLA04"/>
;Flow S
:Small-sized model for lighter pilots. Its {{convert|11.1|m|ft|1|abbr=on}} span wing has a wing area of {{convert|26.2|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.7:1. The pilot weight range is {{convert|70|to|90|kg|lb|0|abbr=on}}. In 2003 the glider model was undergoing certification.<ref name="WDLA04"/>
;Flow M
:Mid-sized model for medium-weight pilots. Its {{convert|11.5|m|ft|1|abbr=on}} span wing has a wing area of {{convert|28.5|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.7:1. The pilot weight range is {{convert|85|to|105|kg|lb|0|abbr=on}}. In 2003 the glider model was undergoing certification.<ref name="WDLA04"/>
;Flow L
:Large-sized model for heavier pilots. Its {{convert|12.1|m|ft|1|abbr=on}} span wing has a wing area of {{convert|31.4|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.7:1. The pilot weight range is {{convert|95|to|125|kg|lb|0|abbr=on}}. In 2003 the glider model was undergoing certification.<ref name="WDLA04"/>
<!-- ==Aircraft on display== -->

==Specifications (Flow M) ==
{{Aircraft specs
|ref=Bertrand<ref name="WDLA04" />
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|crew=one
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|span m=11.6
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|wing area sqm=28.5
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|aspect ratio=4.7:1
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|max speed kmh=44
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==See also==
*[[Zero Gravity Windstar]]

==References==
{{reflist}}

<!-- ==External links== -->
[[Category:Zero Gravity aircraft|Flow]]
[[Category:Paragliders]]