Phoenix Skywalker

{{Short description|German paramotor}} {{Use dmy dates|date=December 2022}} {{Use British English|date=December 2022}}  {{Infobox aircraft | name = Skywalker | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = [[Paramotor]] | aim = | outcome = | related = | national_origin = [[Germany]] | manufacturer = [[Phoenix Gleitschirmantriebe]] | design_group = | designer = | builder = | issuer = | status = Production completed | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} The '''Phoenix Skywalker''' is a series of [[Germany|German]] [[paramotor]]s that was designed and produced by [[Phoenix Gleitschirmantriebe]] of [[Würselen]] for [[powered paragliding]]. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.<ref name="WDLA04">Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', page 73. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X</ref>

==Design and development== The Skywalker 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 2.25:1 ratio [[reduction drive]] and a {{convert|86|cm|in|0|abbr=on}} diameter four-bladed composite propeller. The use of a four-bladed propeller allows a smaller cage size and reduces the overall dimensions of the aircraft. The fuel tank capacity is {{convert|5|L}} and electric start was offered as a factory option.<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"/>  ==Variants== ;Skywalker 210 :Model with a {{convert|18|hp|kW|0|abbr=on}} [[Solo 210]] engine in [[pusher configuration]] with a 2.25:1 ratio [[reduction drive]] and a {{convert|86|cm|in|0|abbr=on}} diameter four-bladed composite propeller. Empty weight is {{convert|23|kg|lb|0|abbr=on}}.<ref name="WDLA04"/> ;Skywalker 330 :Model with a {{convert|22|hp|kW|0|abbr=on}} [[Hirth F-33]] engine in pusher configuration with a 2.25:1 ratio [[reduction drive]] and a {{convert|86|cm|in|0|abbr=on}} diameter four-bladed composite propeller. Empty weight is {{convert|24.5|kg|lb|0|abbr=on}}.<ref name="WDLA04"/>

==Specifications (Skywalker 210) == {{Aircraft specs |ref=Bertrand<ref name="WDLA04"/> |prime units?=met  |genhide=

|crew=one |capacity= |length m= |length ft= |length in= |length note= |span m= |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |fuel capacity={{convert|5|L}} |more general=  |eng1 number=1 |eng1 name=[[Solo 210]] |eng1 type=single cylinder, [[two-stroke]], air-cooled [[aircraft engine]], with a 2.25:1 [[reduction drive]] |eng1 kw= |eng1 hp=18

|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= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |power/mass= |thrust/weight= |more performance= |avionics= }}

==References== {{reflist}}

==External links== *[http://www.flying-directory.com/popup_info.php?action=aircraft&id=40132 Phoenix Skywalker 330 info and image page] [[Category:Phoenix Gleitschirmantriebe aircraft|Skywalker]] [[Category:2000s German ultralight aircraft]] [[Category:Single-engined pusher aircraft]] [[Category:Paramotors]]