TST-13 Junior TeST, spol. s r.o.   


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General Details
Manufacturer: TeST, spol. s r.o.
Plane Name:

TST-13 Junior

Classified as: SLMG
Country Of Origin: Czech Republic
Designer:
No. of Seats 1
No. Built 0
   
Performance:
L/DMax: 24-32 at 93 km/h
   
MinSink:
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
15 0 10.03 0 322.5 0 122.5 0 437 0 0 0 0 0
Aspect ratio: 22.8
Airfoil:
Structure: all-composite structure
Engine: Rotax 447 or Rotax 503

Comment:
TST-13 Junior is a single-seat ultralight composite glider with an engine installed in the front part of the fuselage. The aircraft is suitable for tourist flights and leisure thermal flying. The goal of the development work on the TST-13 was to design an ultralight aircraft for pleasurable flying and to feature aerodynamics to allow utilization of thermal conditions for gliding and motorless flights. The concept of the TST-13 is based on the high-performance TST-10 Atlas glider. We used the same wing span of 15m and the fuselage of the TST-10 was modified to enable the installation of the propulsion unit with a thrust propeller in the front part of the fuselage. The fuselage of the TST-13 features an instrumentation panel and design conforming to the category of ultralight motorless aircraft. The landing gear is fitted with two wheels with a controlled tailwheel.


           

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