190:
31:
114:, introduced c. 1998. When it was available the aircraft was supplied as a completely assembled aircraft, without engine or instruments, and also as a kit for amateur construction.
574:
569:
579:
401:
475:
594:
159:
is intended to give docile handling and is supported by "V"-struts. The standard engine used is the M-125 powerplant.
436:
385:
584:
162:
The manufacturer estimated the construction time from the supplied "express-built" kit as 250 hours.
589:
313:
150 km/h (93 mph, 81 kn) max; 90–120 km/h (56–75 mph; 49–65 kn) economical
468:
248:
130:
564:
200:
AeroCrafter and The
Incomplete Guide to Airfoil Usage, Jane's all the World's Aircraft 2004–05
543:
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146:
138:
8:
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405:
103:
46:
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134:
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2-cylinder 2-stroke liquid-cooled piston engine, 47.8 kW (64.1 hp)
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262:
153:
123:
107:
71:
152:
The aircraft is of all-wood construction. Its constant-chord wing with a
142:
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156:
453:
111:
378:
AeroCrafter - Homebuilt
Aircraft Sourcebook, Fifth Edition
282:
36 L (9.5 US gal; 7.9 imp gal)
174:
Original model with constant chord, strut-braced wing
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184:
556:
431:. London: Jane's Publishing Group. p. 116.
380:, page 362. BAI Communications, 15 July 1998.
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570:1990s Czech and Czechoslovak sport aircraft
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357:
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117:
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328:170 km/h (110 mph, 92 kn)
188:
429:Jane's all the World's Aircraft 2004–05
426:
402:"The Incomplete Guide to Airfoil Usage"
557:
319:65 km/h (40 mph, 35 kn)
457:
13:
232:10.5 m (34 ft 5 in)
180:Model with tapered cantilever wing
106:that was designed and produced by
14:
606:
449:
244:13.7 m (147 sq ft)
226:6.4 m (21 ft 0 in)
483:
238:2.3 m (7 ft 7 in)
29:
580:Single-engined tractor aircraft
346:3.5 m/s (690 ft/min)
298:2-bladed fixed pitch propeller
185:Specifications (TST-5 Variant)
1:
350:
334:4,000 m (13,000 ft)
122:The TST-5 Variant features a
595:Aircraft first flown in 1998
7:
427:Jackson, Paul, ed. (2005).
165:
10:
611:
131:side-by-side configuration
491:
276:450 kg (992 lb)
270:260 kg (573 lb)
133:enclosed cockpit under a
37:
28:
23:
400:Lednicer, David (2010).
16:Czech homebuilt aircraft
205:General characteristics
145:and a single engine in
585:Shoulder-wing aircraft
194:
193:TeST TST-5 Variant Duo
118:Design and development
192:
147:tractor configuration
139:tricycle landing gear
89:Production completed
274:Max takeoff weight:
590:Homebuilt aircraft
324:Never exceed speed
195:
104:homebuilt aircraft
97:TeST TST-5 Variant
47:Homebuilt aircraft
38:TST-5 Variant Duo
552:
551:
177:TST-5 Variant Duo
129:, a two-seats-in-
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92:
602:
544:TST-14J BonusJet
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408:on 20 April 2010
404:. Archived from
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332:Service ceiling:
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58:
50:Type of aircraft
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57:National origin
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450:External links
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344:Rate of climb:
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280:Fuel capacity:
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62:Czech Republic
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26:
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24:TST-5 Variant
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565:TeST aircraft
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534:TST-13 Junior
532:
530:
527:
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509:TST-5 Variant
507:
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504:TST-3 Alpin T
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438:0-7106-2614-2
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386:0-9636409-4-1
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311:Cruise speed:
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268:Empty weight:
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220:one passenger
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171:TST-5 Variant
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135:bubble canopy
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127:shoulder-wing
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78:Introduction
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68:Manufacturer
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41:
36:
32:
27:
22:
19:
539:TST-14 Bonus
529:TST-10 Atlas
524:TST-9 Junior
519:TST-7 Junior
508:
485:TeST Gliders
428:
422:
410:. Retrieved
406:the original
377:
376:Purdy, Don:
343:
337:
331:
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317:Stall speed:
316:
310:
303:
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295:
290:Rotax 582 UL
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249:Aspect ratio
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124:strut-braced
121:
108:TeST Gliders
96:
94:
72:TeST Gliders
18:
499:TST-1 Alpin
304:Performance
296:Propellers:
286:Powerplant:
143:wheel pants
81:circa 1998
559:Categories
351:References
242:Wing area:
514:TST-6 Duo
338:g limits:
263:NACA 4415
230:Wingspan:
218:Capacity:
198:Data from
154:NACA 4415
492:Aircraft
166:Variants
137:, fixed
340:+4 / -2
258:Airfoil
236:Height:
224:Length:
157:airfoil
86:Status
435:
412:11 May
384:
212:Crew:
141:with
101:Czech
99:is a
43:Role
433:ISBN
414:2014
382:ISBN
288:1 ×
112:Brno
95:The
214:one
110:of
561::
392:^
359:^
149:.
477:e
470:t
463:v
441:.
416:.
326::
260::
253:8
251::
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
