TeST TST-13 Junior
| TST-13 Junior | |
|---|---|
| Role | Motor glider |
| National origin | Czech Republic |
| Manufacturer | TeST sro (Division of Comp-Let sro), Velké Meziříĉi |
| Number built | 5 by 2007 |
| Developed from | TeST TST-9 Junior, TeST TST-10 Atlas |
The TeST TST-13 Junior is a single-seat touring motor glider with a nose mounted engine, built by TeST in Czech Republic. It is an all composite design which succeeded the TeST TST-9 Junior motor glider in production, incorporating some features of the TeST TST-10 Atlas sailplane, including its wing.[1]
Development and design
TeST introduced the TST-13 single seat motor glider in 2005 as an all-composite replacement for their wood and composite TST-9. It has a similar layout, front engined and with a high T-tail. The TST-13 shares a similar rear fuselage and tail design and identical wing spars with the all-composite TST-10 single seat sailplane. It is a mid wing design with straight tapered wings which, unlike those of the TST-10, are swept forward 5° at 25% chord. The wing tips carry winglets and there are outboard ailerons, two position flaps and upper surface spoilers.[2]
The fuselage of the TST-13 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 light aircraft style cockpit has a rear hinged, single piece canopy and is placed ahead of the wing leading edge. The TST-13 has a tailwheel undercarriage, with spatted mainwheels on fuselage-mounted, sprung, cantilever legs.[2]
There is a choice of two engines: either a 31 kW (42 hp) Rotax 447 or a 37 kW (50 hp) Rotax 503.[2] The 447 drives a propeller which is only adjustable in pitch on the ground, but that of the 503, geared down 2:1, can be feathered in flight. Feathering improves the best glide ratio from 1:24 to 1:32. The greater power of the Rotax 503 increases the cruising speed by about 10 km/h and the climb rate to about 6 m/s (1,200 ft/min).[3]
Operational history
5 TST-13s had been built by 2007.[2] In mid-2010 2 appeared on civil aircraft registers of European countries west of Russia.[4] The TST-13 is designed to meet the US LSA glider constraints and is S-LSA registerable.[3]
Specifications (Rotax 447 engine)
Data from Jane's All the World's Aircraft 2010/11[2]
General characteristics
- Crew: 1
- Length: 7.45 m (24 ft 5 in)
- Wingspan: 15.00 m (49 ft 3 in)
- Wing area: 10.3 m2 (111 sq ft)
- Aspect ratio: 21.8
- Empty weight: 195 kg (430 lb)
- Max takeoff weight: 300 kg (661 lb) 322 kg (710 lb) with BRS ballistic parachute recovery parachute
- Fuel capacity: 20 L (4.4 Imp gal; 5.3 US gal) standard: can be doubled with interchangeable wing tanks
- Powerplant: 1 × Rotax 447 , 31 kW (42 hp)
- Propellers: 2-bladed ground adjustable pitch SportProp 1600 or similar, 1.60 m (5 ft 3 in) diameter
Performance
- Cruise speed: 160 km/h (99 mph, 86 kn)
- Stall speed: 65 km/h (40 mph, 35 kn) maximum; normal 120 km/h (75 mph; 65 kt)
- Never exceed speed: 200 km/h (120 mph, 110 kn)
- g limits: +4.8/-2.8
- Maximum glide ratio: unpowered, 24[3]
See also
References
- ^ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 137. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c d e Jackson, Paul (2010). Jane's All the World's Aircraft 2010-11. Coulsdon, Surrey: IHS Jane's. p. 177. ISBN 978-0-7106-2916-6.
{{cite book}}: Cite has empty unknown parameter:|coauthors=(help) - ^ a b c Official website
- ^ Partington, Dave (2010). European registers handbook 2010. Air Britain (Historians) Ltd. ISBN 978-0-85130-425-0.
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External links
