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136:. Renard designed a low-winged monoplane of all-metal construction, powered by three engines as required by SABENA, and received an order for a single prototype on 3 April 1936. The R.35 had a circular section fuselage, housing a pressurised cabin which accommodated twenty passengers and a flight crew of three. It was intended to be powered by a range of radial engines with the 950 hp (709 kW)
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to return to the runway, the R.35 dived into the ground and was destroyed, killing the pilot
Georges Van Damme. The cause of the crash was unknown. Following this crash, SABENA abandoned its interest in the R.35, and Renard abandoned development.
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airfield in front of an audience of visiting dignitaries and journalists. After carrying out a single taxi-run, however, the R.35 took off during a second run, and while attempting a
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Hauet, André (January 1977). "Il devait donner la stratosphère à la
Belgique... Renard R.35" [It was to Give the Stratosphere to Belgium... Renard R.35].
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In 1935, Alfred Renard, chief designer and co-founder of the Renard company, started design of a pressurised airliner for use by
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The R.35 was completed early in 1938. On 1 April 1938, it was planned to carry out high-speed taxiing trials at
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with retractable undercarriage, the R.35 was destroyed in a crash on its first flight.
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Proposed bomber version, capable of carrying 2,800 kg (6,200 lb) of bombs. Unbuilt.
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preferred by Renard, but the prototype was fitted with 750 hp (560 kW)
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425:, September 1978, Vol 15 No. 3. Bromley, UK: Fine Scroll. pp. 147–149.
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435 km/h (270 mph, 235 kn) at 5,000 ft (1,500 m)
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Renard R.35 Un avion stratosphérique belge en 1938. (technique)
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Renard R.35 Un avion stratosphérique belge en 1938. (histoire)
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ASN Aircraft accident 01-APR-1938 Renard R.35 OO-ARM
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397:. 15 April 2009. Retrieved 26 August 2009.
282:350 km/h (220 mph, 190 kn)
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419:De Wulf, Herman. "A Belgian Rare Avis".
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354:. (In French). Retrieved 26 August 2009.
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173:Specifications (performance estimated)
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109:Constructions Aéronautiques G. Renard
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217:17.50 m (57 ft 5 in)
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229:5.50 m (18 ft 1 in)
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261:, 560 kW (750 hp) each
235:87 m (940 sq ft)
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247:10,500 kg (23,149 lb)
194:3 (2 pilots and radio operator)
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241:6,100 kg (13,448 lb)
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294:9,000 m (30,000 ft)
209:2,000 kg (4,400 lb)
607:Aircraft first flown in 1938
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318:De Wulf 1978, pp. 147-148.
102:of the 1930s built by the
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433:(in French) (86): 14–17.
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592:1930s Belgian airliners
395:Aviation Safety Network
185:General characteristics
257:9-cylinder air-cooled
124:Development and design
106:aircraft manufacturer
493:Aircraft produced by
431:Le Fana de l'Aviation
132:on its routes to the
406:De Wulf 1978, p.149.
363:De Wulf 1978, p.147.
334:De Wulf 1978, p.148.
180:A Belgian Rare Avis
245:Max takeoff weight:
602:Low-wing aircraft
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81:Number built
458:RENARD R-35
378:Aérostories
352:Aérostories
267:Performance
251:Powerplant:
116:low-winged
97:pressurised
93:Renard R.35
581:Categories
301:References
233:Wing area:
597:Trimotors
439:0757-4169
221:Wingspan:
198:Capacity:
178:Data from
144:engines.
118:monoplane
64:Designer
506:Epervier
160:Variants
100:airliner
49:Belgium
36:Airliner
227:Height:
215:Length:
153:circuit
104:Belgian
495:Renard
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286:Range:
130:SABENA
58:Renard
453:photo
306:Notes
192:Crew:
165:R.35B
149:Evere
112:. A
33:Role
19:R.35
566:R.40
561:R.38
556:R.37
551:R.36
546:R.35
541:R.34
536:R.33
531:R.32
526:R.31
521:R.30
516:R.17
511:R.16
435:ISSN
253:3 ×
91:The
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205:or
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