TeST TST-9 Junior

{{Short description|Czech motorglider}}

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

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

{{Infobox aircraft begin

| name=TST-9 Junior

| image=

| caption=

}}{{Infobox aircraft type

| type=Motor glider

| national origin=Czech Republic

| manufacturer=TeST

| designer=

| first flight=

| introduced=

| retired=

| status=Production completed

| primary user=

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| developed from= TeST TST-7 Junior

| variants with their own articles=TeST TST-13 Junior

}}

The TeST TST-9 Junior is a Czech shoulder-wing, single-seat motor glider that was designed and produced by TeST of Brno. When it was available the aircraft was supplied as plans, in kit form for amateur construction or as a complete ready-to-fly aircraft. Production is now complete and the aircraft is no longer available.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 59. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}

Design and development

The TST-9 Junior was a development of the TST-7 Junior touring motor glider, incorporating a T-tail and other design refinements. The {{convert|12.4|m|ft|1|abbr=on}} span, shoulder-mounted wing is slightly forward-swept. The wing has less span than the TST-7 Junior and consequently the aircraft has a lower glide ratio. The landing gear is of tricycle configuration, making taxiing the aircraft much easier than the monowheel gear used on the TST-1 model. The aircraft was later further refined into the TST-13 Junior.

The price for a completed ready-to-fly aircraft in 2004 was 22,240.

Specifications (TST-9 Junior)

{{Aircraft specs

|ref=World Directory of Leisure Aviation, Jane's all the World's Aircraft 2004–05{{cite book |title=Jane's all the World's Aircraft 2004–05 |editor1-last=Jackson |editor1-first=Paul |year=2005 |publisher=Jane's Publishing Group |location=London |isbn=0-7106-2614-2|page=117}}

|prime units?=met

|crew=one

|capacity=

|length m=5.9

|span m=12.4

|height m=2.1

|wing area sqm=10

|aspect ratio=15.4

|airfoil=

|empty weight kg=175

|gross weight kg=

|gross weight lb=

|gross weight note=

|max takeoff weight kg=300

|fuel capacity={{convert|25|L|USgal impgal|abbr=on}}

|more general=

|eng1 number=1

|eng1 name=Rotax 447

|eng1 type=two stroke aircraft engine

|eng1 kw=

|eng1 hp=

|prop blade number=2

|prop name=SportProp 1600

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=

|max speed mph=

|max speed kts=

|max speed note=

|cruise speed kmh=165

|cruise speed note=max; {{convert|90|-|120|km/h|mph kn|abbr=on}} economical

|stall speed kmh=63

|stall speed note=in the landing configuration

|never exceed speed kmh=180

|range km=

|range miles=

|range nmi=

|range note=

|endurance=

|ceiling m=5000

|g limits=+4 / -2

|roll rate=

|glide ratio=20:1 at {{convert|90|km/h|mph kn|0|abbr=on}}

|climb rate ms=

|climb rate ftmin=900

|climb rate note=

|sink rate ms=1.5

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|more performance=

|avionics=

}}

See also

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References

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