TeST TST-14J BonusJet

{{Infobox Aircraft Begin

| name=TST-14J BonusJet

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Motor glider

| national origin=Czech Republic

| manufacturer=TeST sro (Division of Comp-Let sro), Velké Meziříĉi, Desert Aerospace, LLC

| designer=

| first flight=

| introduced=

| retired=

| status=

| primary user=

| more users=

| produced=

| number built=

| program cost=

| unit cost=

| developed from=TeST TST-14 Bonus

| variants with their own articles=

}}

The TeST TST-14J BonusJet is a two-seat touring motor glider with a retractable PBS TJ-100 turbine engine, built by TeST in the Czech Republic. It is an all composite design.{{cite news|newspaper=Fly-Low|date=July 2010}}

Development and design

The TST-14J is a Desert Aerospace, LLC modification of the TST-14 motorglider with the addition of a retractable jet engine used for self launching. It has a high T-tail. It is a mid wing design with straight tapered wings. The wing tips carry winglets and there are outboard ailerons, two position flaps and upper surface spoilers.{{cite web|title=Desert Aerospace|url=http://www.desertaerospace.com/bonusjet/bonus_info.html|accessdate=13 August 2011}}

The fuselage of the TST-14J is built from two half shells which incorporate the straight tapered fin. The fuselage tapers rearwards, producing an arched shape below. The tailplane carries a single piece elevator. The cockpit has a forward hinged, single piece canopy, and a side hinged passenger canopy. The TST-14J has a tailwheel undercarriage, with spatted mainwheels on fuselage-mounted, sprung, cantilever legs.

The 45 lb PBS TJ-100 turbine engine {{Cite web|title=TST-14J BonusJet|url=http://www.switched.com/2010/08/10/tst-14j-bonusjet-comes-with-retractable-jet-engine/|accessdate=13 August 2011}} requires a two-minute cooldown before retracting into the fuselage. The prototype was tested by Bob Carlton, an experienced jet powered glider pilot who flies an aerobatic routine in a Super Salto jet powered glider with the same engine.{{cite web|title=Jet Powered glider tested|url=http://www.aopa.org/aircraft/articles/2010/100607desertaerospace.html|accessdate=13 August 2011}} Sonex Aircraft also uses the same engine, and hired Carlton to test its SubSonex jet-powered homebuilt aircraft.

Specifications

{{Aircraft specs

|ref=Fly-Low

|prime units?=met

|genhide=

|crew=2

|capacity=

|length m=

|length ft=

|length in=

|length note=

|span m=17

|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=

|empty weight lb=

|empty weight note=

|gross weight kg=

|gross weight lb=

|gross weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=První Brnenská Strojírna PBS TJ-100

|eng1 type=

|eng1 kw=

|eng1 hp=

|eng1 kn=1

|eng1 lbf=

|eng1 note=

|power original=

|thrust original=

|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=

|stall speed kmh=65

|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}}