MS Parafly Skyward
{{Short description|German paramotor}}
{{Use dmy dates|date=December 2022}}
{{Use British English|date=December 2022}}
| {{Infobox Aircraft Begin
| name=Skyward | image= | caption= }}{{Infobox Aircraft Type | type=Paramotor | national origin=Germany | manufacturer=MS Parafly | designer=Martin Sauter | first flight= | introduced= | retired= | status=Production completed | primary user= | more users= | produced= 2001-2005 | number built= | developed from= | variants with their own articles= }} |
The MS Parafly Skyward is a family of German paramotors that was designed by Martin Sauter and produced by MS Parafly of Meßstetten for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 70. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
Design and development
The Skyward line 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 engine in pusher configuration with a reduction drive and a {{convert|111|to|124|cm|in|0|abbr=on}} diameter two-bladed composite propeller, depending on the model. The aircraft is noted for its low noise.
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.
Variants
;Skyward 1
:Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a {{convert|111|cm|in|0|abbr=on}} diameter two-bladed composite propeller. Empty weight is {{convert|20|kg|lb|0|abbr=on}}. The fuel tank capacity is {{convert|8.5|L}}.
;Skyward 2
:Model with a {{convert|20|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a {{convert|111|cm|in|0|abbr=on}} diameter two-bladed composite propeller. Empty weight is {{convert|22|kg|lb|0|abbr=on}}. The fuel tank capacity is {{convert|8.5|L}}.{{cite web|url=http://msparafly.de/page3.html|archiveurl=https://web.archive.org/web/20050205030417/http://msparafly.de/page3.html|title=Skyward 2|archivedate=5 February 2005|work=msparafly.de|accessdate=3 November 2015}}
;Skyward 3
:Model with a {{convert|20|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a {{convert|124|cm|in|0|abbr=on}} diameter two-bladed composite propeller. Empty weight is {{convert|23|kg|lb|0|abbr=on}}. The fuel tank capacity is {{convert|8.5|L}}.{{cite web|url=http://msparafly.de/page4.html|archiveurl=https://web.archive.org/web/20050205030503/http://msparafly.de/page4.html|title=Skyward 3|archivedate=5 February 2005|work=msparafly.de|accessdate=3 November 2015}}
;Skyward Mini
:Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a direct drive and an {{convert|80|cm|in|0|abbr=on}} diameter two-bladed composite propeller. Empty weight is {{convert|14|kg|lb|0|abbr=on}}. The fuel tank capacity is {{convert|5|L}}.{{cite web|url=http://msparafly.de/page2.html|archiveurl=https://web.archive.org/web/20050205025452/http://msparafly.de/page2.html|title=Skyward Mini|archivedate=5 February 2005|work=msparafly.de|accessdate=3 November 2015}}
Specifications (Skyward 1)
{{Aircraft specs
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|eng1 number=1
|eng1 name=Solo 210
|eng1 type=single cylinder, two-stroke, air-cooled aircraft engine, with a 2.5:1 reduction drive
|eng1 kw=
|eng1 hp=14
|prop blade number=2
|prop name=composite, fixed pitch
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