164:, interrupting the aircraft's test programme, it having flown 41 hours 18 minutes by this time. The evacuation was not successful, as the NC.130 was destroyed later that year.
121:
In order to aid the design of these projects and, in particular, the pressure cabins that they needed, SNCAC designed a pressurised twin-engined research aircraft, the
106:) in 1936, SNCAC continued its interest in high altitude aircraft, proposing a number of high-altitude projects, including the NC.140 four-engined heavy bomber (a
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pressure cabin in the nose of the aircraft, with the pilot provided with thick glass portholes in the upper part of the cabin to allow outward vision.
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was a French high-altitude research aircraft of the 1930s. A single example flew in 1939, but was destroyed during the
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404:
Liron, Jean; Passingham, Malcolm (May 1970). "French
Projects—1940: Part 3: S.N.C.A.C. & S.N.C.A.O".
445:
693:
647:
626:
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Liron, Jean; Passingham, Malcolm (April 1970). "French
Projects—1940: Part 2: Delanne to S.N.C.A.C.".
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series of high altitude aircraft in the early 1930s. When Farman was nationalised to form part of the
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The NC.130 made its maiden flight on 10 October 1939. In May 1940, it was evacuated to the former
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engines. Its crew of three were accommodated in a cylindrical riveted
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Société Nationale de
Constructions Aéronautiques du Centre (SNCAC)
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Borget, Michel (April 2002). "Le défi à l'altitude du NC.130".
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Aircraft of comparable role, configuration, and era
136:. It was powered by two 720 hp (540 kW)
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248:300.0 km/h (186.4 mph, 162.0 kn)
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408:. Vol. 32, no. 5. pp. 170–172.
399:. Vol. 32, no. 4. pp. 130–133.
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390:(in French). No. 389. pp. 24–34.
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213:40.30 m (433.8 sq ft)
201:16.63 m (54 ft 7 in)
195:11.75 m (38 ft 7 in)
13:
684:1930s French experimental aircraft
207:4.19 m (13 ft 9 in)
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233:, 540 kW (730 hp) each
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90:The French aircraft manufacturer
254:10,600 m (34,776 ft)
125:. The NC.130 was a low-winged
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704:Twin-engined tractor aircraft
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219:4,501 kg (9,922 lb)
699:Aircraft first flown in 1939
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10:
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180:General characteristics
134:tailwheel undercarriage
114:) and the twin-engined
94:designed and built the
86:Design and development
388:Le Fana de l'Aviation
368:Liron and Passingham
297:Liron and Passingham
175:French Projects—1940
345:"S.N.C.A.C. NC-130"
343:Parmentier, Bruno.
301:April 1970, p. 133.
227:Hispano-Suiza 12Ybr
148:Operational history
138:Hispano-Suiza 12Ybr
110:derivative of the
694:Low-wing aircraft
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372:May 1970, p. 172.
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27:Research aircraft
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58:10 October 1939
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29:Type of aircraft
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36:National origin
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315:"SNCAC NC.130"
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246:Maximum speed:
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168:Specifications
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160:to escape the
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653:Chardonneret
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352:. Retrieved
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322:. Retrieved
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156:airfield at
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123:SNCAC NC.130
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76:SNCAC NC.130
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64:Number built
354:28 December
324:28 December
319:Уголок Неба
239:Performance
231:V12 engines
223:Powerplant:
108:pressurised
678:Categories
380:References
349:Aviafrance
211:Wing area:
127:cantilever
648:Belphégor
455:by number
199:Wingspan:
173:Data from
142:duralumin
130:monoplane
663:Martinet
658:Cormoran
259:See also
118:bomber.
643:Abeille
636:by name
627:NC.3021
612:NC.2001
607:NC 1080
602:NC.1071
597:NC.1070
507:NC.47-2
502:NC.47-1
497:NC.47-0
482:NC.4-10
205:Height:
193:Length:
158:Bourges
154:Hanriot
40:France
19:NC.130
622:NC.271
617:NC 211
592:NC.900
587:NC.860
582:NC.856
577:NC.855
572:NC.854
567:NC.853
562:NC.851
557:NC.850
552:NC.841
547:NC.840
542:NC.832
537:NC.702
532:NC.701
527:NC.700
522:NC.600
517:NC.530
512:NC.510
492:NC.433
487:NC.420
477:NC.223
472:NC.211
467:NC.150
462:NC.130
116:NC.150
92:Farman
278:Notes
187:Crew:
104:SNCAC
24:Role
356:2012
326:2012
225:2 ×
74:The
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68:1
439:e
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189:3
102:(
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