Alliant Destiny XLT

{{Infobox aircraft | name = Destiny XLT | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = [[Powered parachute]] | aim = | outcome = | related = | national_origin = [[United States]] | manufacturer = [[Alliant Aviation]] | design_group = | designer = | builder = | issuer = | status = | 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 '''Alliant Destiny XLT''' is an American two-seat [[powered parachute]], designed and produced by [[Alliant Aviation]] based at [[Richland, Michigan]].<ref name="wdla04" />

==Design and development== The aircraft was designed to comply with the FAI Microlight rules. It features a [[parachute]]-style [[high-wing]] and two-seats in tandem in an open frame, [[tricycle landing gear]] and a single {{convert|64|hp|kW|0|abbr=on}} [[Rotax 582]] engine in [[pusher configuration]]. Versions were also available with a [[Rotax 503]] or [[Hirth 3701]] engine.<ref name="wdla04" />

==Variants== ;ST :Single-seat variant ;LT :Two-seat lightweight variant ;XLT :Heavier two-seat variant

==Specifications (XLT with Rotax 582) == {{Aircraft specs |ref={{small|World Directory of Leisure Aviation 2004/2005}}<ref name="wdla04" /> |prime units?=imp  |genhide= |crew=two |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=175 |empty weight lb= |empty weight note= |gross weight kg=450 |gross weight lb= |gross weight note= |fuel capacity= |more general=  |eng1 number=1 |eng1 name=[[Rotax 582]] |eng1 type=twin cylinder, [[two-stroke]], liquid-cooled [[aircraft engine]] |eng1 kw= |eng1 hp=64 |prop blade number=3 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note=

|perfhide= |max speed kmh=55 |max speed mph= |max speed kts= |max speed note= |cruise speed kmh=52 |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= }}

{{aircontent  |see also= |related= |similar aircraft= |lists= }}

==References== <references>

<ref name="wdla04">{{cite journal | title = World Directory of Leisure Aviation 2004/2005 |journal= World Directory of Light Aviation|publisher = Pagefast Ltd, England | year = 2004 | page= 77 |issn = 1368-485X}}</ref>

</references>

{{Alliant Aviation aircraft}}

[[Category:2000s United States ultralight aircraft]] [[Category:Single-engined pusher aircraft]] [[Category:Powered parachutes]] [[Category:Alliant aircraft]]