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{{Short description|German paramotor}}
{{Use dmy dates|date=December 2022}}
{{Use British English|date=December 2022}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{|{{Infobox Aircraft Begin
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| produced= 2001-2005
| produced= 2001-2005
| number built=
| number built=
| program cost= <!--Total program cost-->
| unit cost= [[Euro|€]]2,370 (Skyward 1, 2004)
| developed from=
| developed from=
| variants with their own articles=
| variants with their own articles=
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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.<ref name="WDLA04"/>
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.<ref name="WDLA04"/>
<!-- ==Operational history== -->
<!-- ==Operational history== -->

==Variants==
==Variants==
;Skyward 1
;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}}.<ref name="WDLA04"/>
: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}}.<ref name="WDLA04"/>
;Skyward 2
;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}}.<ref name="WDLA04"/><ref>{{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}}</ref>
: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}}.<ref name="WDLA04"/><ref>{{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}}</ref>
;Skyward 3
;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}}.<ref name="WDLA04"/><ref>{{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}}</ref>
: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}}.<ref name="WDLA04"/><ref>{{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}}</ref>
;Skyward Mini
;Skyward Mini
:Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a direct drive and a {{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}}.<ref>{{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}}</ref>
:Model with a {{convert|14|hp|kW|0|abbr=on}} Solo 210 engine in pusher configuration with a direct drive and a {{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}}.<ref>{{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}}</ref>
<!-- ==Aircraft on display== -->
<!-- ==Aircraft on display== -->


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|gross weight lb=
|gross weight lb=
|gross weight note=
|gross weight note=
|fuel capacity={{convert|8.5|l}}
|fuel capacity={{convert|8.5|L}}
|more general=
|more general=
<!--
<!--
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<!-- ==External links== -->
<!-- ==External links== -->
[[Category:MS Parafly aircraft|Skyward]]
[[Category:MS Parafly aircraft|Skyward]]
[[Category:German ultralight aircraft 2000–2009]]
[[Category:2000s German ultralight aircraft]]
[[Category:Single-engine aircraft]]
[[Category:Single-engined pusher aircraft]]
[[Category:Paramotors]]
[[Category:Paramotors]]

Latest revision as of 20:57, 9 December 2022

Skyward
Role Paramotor
National origin Germany
Manufacturer MS Parafly
Designer Martin Sauter
Status Production completed
Produced 2001-2005

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.[1]

Design and development

[edit]

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 111 to 124 cm (44 to 49 in) diameter two-bladed composite propeller, depending on the model. The aircraft is noted for its low noise.[1]

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.[1]

Variants

[edit]
Skyward 1
Model with a 14 hp (10 kW) Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a 111 cm (44 in) diameter two-bladed composite propeller. Empty weight is 20 kg (44 lb). The fuel tank capacity is 8.5 litres (1.9 imp gal; 2.2 US gal).[1]
Skyward 2
Model with a 20 hp (15 kW) Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a 111 cm (44 in) diameter two-bladed composite propeller. Empty weight is 22 kg (49 lb). The fuel tank capacity is 8.5 litres (1.9 imp gal; 2.2 US gal).[1][2]
Skyward 3
Model with a 20 hp (15 kW) Solo 210 engine in pusher configuration with a 2.5:1 ratio reduction drive and a 124 cm (49 in) diameter two-bladed composite propeller. Empty weight is 23 kg (51 lb). The fuel tank capacity is 8.5 litres (1.9 imp gal; 2.2 US gal).[1][3]
Skyward Mini
Model with a 14 hp (10 kW) Solo 210 engine in pusher configuration with a direct drive and a 80 cm (31 in) diameter two-bladed composite propeller. Empty weight is 14 kg (31 lb). The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal).[4]

Specifications (Skyward 1)

[edit]

Data from Bertrand[1]

General characteristics

  • Crew: one
  • Empty weight: 20 kg (44 lb)
  • Fuel capacity: 8.5 litres (1.9 imp gal; 2.2 US gal)
  • Powerplant: 1 × Solo 210 single cylinder, two-stroke, air-cooled aircraft engine, with a 2.5:1 reduction drive, 10 kW (14 hp)
  • Propellers: 2-bladed composite, fixed pitch, 1.11 m (3 ft 8 in) diameter

References

[edit]
  1. ^ a b c d e f g Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 70. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
  2. ^ "Skyward 2". msparafly.de. Archived from the original on 5 February 2005. Retrieved 3 November 2015.
  3. ^ "Skyward 3". msparafly.de. Archived from the original on 5 February 2005. Retrieved 3 November 2015.
  4. ^ "Skyward Mini". msparafly.de. Archived from the original on 5 February 2005. Retrieved 3 November 2015.
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