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166:, though the cylinders protruded for cooling. Later, this engine was replaced by a 60 hp (45 kW), five cylinder
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700 km (430 mi, 380 nmi) ; 1,300 km (810 mi; 700 nmi) with overload fuel
656:
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mounted in the short nose section. This was carefully streamlined and integrated smoothly with the
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was positioned on top of the fuselage and braced from below with two parallel struts. The
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201:, was hinged on a pair of V-form struts to the central fuselage with a vertical, faired
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fuselage. It was initially powered by a 65 hp (48 kW), three cylinder
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pylon and braced to the lower fuselage on each side by a V-form pair of faired
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was almost triangular though it rounded at the top into a broad, curved, deep
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radial, the same type used by the G-8, which slightly lightened the aircraft.
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Although the G-10 incorporated many structural feature from the earlier
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181:, from which the pilot could see both below and above the wing. The
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and later in its career had the same engine, it was a braced
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382:. London: Osprey (Reed Consumer Books Ltd). p. 78.
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which extended down to the keel. The G-10 had a fixed
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140:Like the G-8, the G-10 had a smoothly rounded,
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410:Russian Civil and Military Aircraft 1884-1969
197:; each of the main wheels, enclosed in broad
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455:
441:
173:The G-10 had a large cut-out in the wing
100:
319:170 km/h (110 mph, 92 kn)
226:
377:
205:from the axle to the central fuselage.
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462:
403:
401:
399:
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337:11 min to 2,000 m (6,560 ft)
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408:Nowarra, Norman; Duval, G.R. (1971).
219:or Central Moscow Airfield) in 1933.
125:wing was supported over the central
609:Known projects and unflown aircraft
396:
360:
13:
14:
673:
264:8.4 m (27 ft 7 in)
258:5.6 m (18 ft 4 in)
270:11 m (120 sq ft)
212:(the state aviation factory at
1:
353:
331:5,200 m (17,100 ft)
662:Aircraft first flown in 1933
223:Specifications (M-23 engine)
208:The G-10 was constructed at
7:
647:1930s Soviet sport aircraft
282:510 kg (1,124 lb)
10:
678:
93:designed and built in the
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547:
471:
298:, 48 kW (65 hp)
276:335 kg (739 lb)
86:
18:
343:100 m (330 ft)
288:75 kg (165 lb)
121:design. The G-10's two
113:monoplane rather than a
472:Powered aircraft, flown
349:80 m (260 ft)
243:General characteristics
195:tail skid undercarriage
378:Gunston, Bill (1995).
232:
101:Design and development
230:
294:1 ร M-23 3-cylinder
97:in the early 1930s.
89:) was a single seat
53:Vladislav Gribovsky
238:Gunston (1995) p.78
657:High-wing aircraft
652:Gribovsky aircraft
412:. Fountain Press.
341:Take-off distance:
233:
217:Khodynka Aerodrome
634:
633:
347:Landing distance:
335:Time to altitude:
191:unbalanced rudder
162:of the two blade
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329:Service ceiling:
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88:
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32:Type of aircraft
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129:on a very low,
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91:sports aircraft
87:ะะ ะะะะะกะะะ ะ-10
66:
39:National origin
38:
33:
29:sports aircraft
19:Gribovsky G-10
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548:Gliders, flown
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317:Maximum speed:
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286:Fuel capacity:
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231:Gribovsky G-10
224:
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203:shock absorber
177:over the open
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79:Gribovsky G-10
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389:1-85532-405-9
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296:radial engine
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280:Gross weight:
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274:Empty weight:
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175:trailing edge
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156:radial engine
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107:Gribovsky G-8
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58:First flight
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168:Walter NZ-60
139:
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78:
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67:Number built
27:Single seat
310:Performance
302:Propellers:
292:Powerplant:
641:Categories
575:G-11 (VVS)
354:References
268:Wing area:
119:cantilever
464:Gribovsky
262:Wingspan:
236:Data from
183:tailplane
164:propeller
146:monocoque
111:high wing
50:Designer
466:aircraft
304:2-bladed
144:skinned
127:fuselage
115:low wing
256:Length:
179:cockpit
160:spinner
150:Russian
142:plywood
83:Russian
416:
386:
323:Range:
214:Moscow
135:struts
131:faired
626:Dosav
539:G-30M
250:Crew:
210:GAZ-1
199:spats
61:1933
24:Role
600:G-31
595:G-29
590:G-16
585:G-14
580:G-12
534:G-28
529:G-27
524:G-26
519:G-25
514:G-23
509:G-22
504:G-21
499:G-20
494:G-15
489:G-10
414:ISBN
384:ISBN
153:M-23
123:spar
95:USSR
77:The
44:USSR
621:G-4
616:G-3
570:G-9
565:G-6
560:G-2
555:G-1
484:G-8
479:G-5
252:One
187:fin
643::
398:^
362:^
137:.
117:,
85::
71:1
456:e
449:t
442:v
422:.
392:.
81:(
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