Trixy Liberty

{{Infobox Aircraft Begin

| name= Liberty

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Autogyro

| national origin=Austria

| manufacturer=Trixy Aviation Products

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2017)

| primary user=

| more users=

| produced=

| number built=

| program cost=

| unit cost= 47,775 (2015)

| developed from=

| variants with their own articles=

}}

The Trixy Liberty is an Austrian autogyro designed and produced by Trixy Aviation Products of Dornbirn. The aircraft is supplied complete and ready-to-fly.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 200. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The Liberty was designed as an entry-level, open cockpit gyroplane, although it has an optional cabin canopy enclosure. It features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear without wheel pants, plus a tail caster and a four-cylinder, liquid and air-cooled, four stroke {{convert|100|hp|kW|0|abbr=on}} Rotax 912 or turbocharged {{convert|115|hp|kW|0|abbr=on}} Rotax 914 engine in pusher configuration.

The aircraft fuselage is made from composites. Its two-bladed rotor has a diameter of {{convert|8.4|m|ft|1|abbr=on}}. The aircraft has a typical empty weight of {{convert|245|kg|lb|0|abbr=on}} and a gross weight of {{convert|560|kg|lb|0|abbr=on}}, giving a useful load of {{convert|315|kg|lb|0|abbr=on}}.

Unlike many other autogyro builders, Trixy Aviation uses a swash plate in its rotor head designs, rather than a tilt head. This makes the design more sensitive to fly and requires special type training.

Specifications (Liberty)

{{Aircraft specs

|ref=Tacke and manufacturer{{cite web|url = http://www.trixyaviation.com/liberty.html|title = Technical data|accessdate = 27 November 2017|author=Trixy Aviation Products |work =trixyaviation.com }}

|prime units?=met

|genhide=

|crew=one

|capacity=one passenger

|length m=4.9

|length ft=

|length in=

|length note=

|width m=1.88

|width ft=

|width in=

|width note=

|height m=2.8

|height ft=

|height in=

|height note=

|airfoil=

|empty weight kg=

|empty weight lb=

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Rotax 912ULS

|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine

|eng1 kw=

|eng1 hp=100

|prop blade number=3

|prop name=composite

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|rot number=1

|rot dia m=8.4

|rot dia ft=

|rot dia in=

|rot area sqm=55

|rot area sqft=

|rot area note=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise 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=8000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=4

|climb rate ftmin=

|climb rate note=

|time to altitude=

|disk loading kg/m2=10.2

|disk loading lb/sqft=

|disk loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

|thrust/weight=

|more performance=

|avionics=

}}

See also

References

{{reflist}}