Alliant Destiny XLT

{{Infobox aircraft begin

| name=Destiny XLT

| image=

| caption=

}}{{Infobox aircraft type

| type=Powered parachute

| national origin=United States

| manufacturer=Alliant Aviation

| designer=

| first flight=

| introduced=

| retired=

| status=

| primary user=

| more users=

| produced=

| number built=

| program cost=

| unit cost= US$16,050 (2004 with Rotax 582)

| developed from=

| variants with their own articles=

}}

The Alliant Destiny XLT is an American two-seat powered parachute, designed and produced by Alliant Aviation based at Richland, Michigan.

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.

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}}

|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

{{reflist|refs=

{{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}}

}}

{{Alliant Aviation aircraft}}

Category:2000s United States ultralight aircraft

Category:Single-engined pusher aircraft

Category:Powered parachutes

Category:Alliant aircraft