DTA Magic

{{Short description|French ultralight trike}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox aircraft begin

| name=Magic

| image=Aerosport 2013 (Igualada) EC-GE2 (aircraft).JPG

| caption=Magic wing mounted on a DTA Feeling

}}{{Infobox aircraft type

| type=Ultralight trike wing

| national origin=France

| manufacturer=DTA sarl

| designer=

| first flight=

| introduced=2010

| retired=

| status= In production (2013)

| primary user=

| more users=

| produced= 2010-present

| number built=

| developed from=

| variants with their own articles=

}}

The DTA Magic is a French double-surface ultralight trike wing, designed and produced by DTA sarl of Montélimar and introduced in 2010. The trike wing was the first "topless" design to be offered by a French manufacturer.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 208-210. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X

Design and development

The Magic is a strut-braced "topless" hang glider-style wing designed as a touring wing for two-place trikes. It comes in one size with a wing area of {{convert|12.0|m2|sqft|abbr=on}}. The wing is comparatively small in area, which gives a higher cruise speed. Its low drag design means that trikes equipped with this wing require less installed power.

The wing is made from bolted-together aluminum tubing, with its 84% double surface wing covered in Dacron sailcloth. Its {{convert|9.4|m|ft|1|abbr=on}} span wing has a nose angle of 130°, an aspect ratio of 6.4:1 and uses an "A" frame weight-shift control bar. The wing tips feature small winglets. It is manufactured by DTA's subcontractor, La société Ellipse.{{cite web|url = http://www.dta.fr/FR/Ailes/Magic/Magic.shtml|title = Magic|accessdate = 2 June 2013|last = DTA sarl|year = 2009|archive-url = https://web.archive.org/web/20120707065144/http://www.dta.fr/FR/Ailes/Magic/Magic.shtml|archive-date = 7 July 2012|url-status = dead}}

Applications

Specifications (Magic 12)

{{Aircraft specs

|ref=Bayerl and DTA

|prime units?=met

|genhide=

|crew=

|capacity=

|length m=2.68

|length ft=

|length in=

|length note=

|span m=9.40

|span ft=

|span in=

|span note=

|height m=1.80

|height ft=

|height in=

|height note=

|wing area sqm=12.0

|wing area sqft=

|wing area note=

|aspect ratio=6.4:1

|airfoil=

|empty weight kg=59

|empty weight lb=

|empty weight note=wing weight

|gross weight kg=450

|gross weight lb=

|gross weight note=maximum aircraft gross weight allowed

|more general=

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|max speed kmh=

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=

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|stall speed kmh=53

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=180

|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=+4/-2

|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=37.5

|wing loading lb/sqft=

|wing loading note=maximum

|more performance=

}}

References

{{reflist}}