Airborne Outback

{{Infobox Aircraft Begin

| name=Outback

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Ultralight trike

| national origin=Australia

| manufacturer=Airborne Windsports

| designer=

| first flight=

| introduced=

| retired=

| status=Production completed

| primary user=

| more users=

| produced=

| number built=

| program cost=

| unit cost=

| developed from=

| variants with their own articles=Airborne XT

}}

The Airborne Outback is an Australian two-seat flying wing ultralight trike that was designed and produced by Airborne Windsports in the mid-2000s.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, pages 22-23. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X

Design and development

The Outback was developed as an off-airport aircraft, with a carriage that lacks a fairing and other encumbrances to "all-terrain" operations. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.

The aircraft single surface Wizard model wing is made from bolted-together aluminium tubing, covered in Dacron sailcloth. Its {{convert|9.96|m|ft|1|abbr=on}} span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The landing gear has optional tundra tires. The standard engine factory-supplied was the Rotax 582 liquid-cooled two-stroke powerplant of {{convert|48|kW|hp|0|abbr=on}}. The aircraft has demonstrated operations from sand dunes.

The basic Outback model was later developed into the Airborne XT series that still dominates the company's product line in 2012.

Specifications (Outback)

{{Aircraft specs

|ref=Bertrand

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=

|length ft=

|length in=

|length note=

|span m=9.96

|span ft=

|span in=

|span note=

|height m=

|height ft=

|height in=

|height note=

|wing area sqm=17.6

|wing area sqft=

|wing area note=

|aspect ratio=

|airfoil=

|empty weight kg=165

|empty weight lb=

|empty weight note=

|gross weight kg=401

|gross weight lb=

|gross weight note=

|fuel capacity={{convert|48|L}}

|more general=

|eng1 number=1

|eng1 name=Rotax 582

|eng1 type=twin cylinder, two-stroke, liquid-cooled aircraft engine

|eng1 kw=48

|eng1 hp=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=93

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=67

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=52

|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=4

|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