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Renard R.30

From Wikipedia, the free encyclopedia
R.30
Role Airliner
National origin Belgium
Manufacturer Renard
First flight 1931
Number built 1

The Renard R.30 was a prototype trimotor airliner built in Belgium in 1931.[1] It was a strut-braced high-wing monoplane of conventional design with a fully enclosed flight deck and separate passenger compartment.[2] One engine was mounted on the nose, while the other two were mounted on the leading edges of the wings.[2] Construction was metal throughout, skinned in plywood and fabric.[2]

The R.30 was designed in response to a Belgian government requirement of 1929 for a long-range passenger transport aircraft to service Belgian Congo.[2] The design met the specifications laid down, but by the time it flew in 1931, it was judged already obsolete.[2] The single prototype, registered OO-AMK, was the only example built.[2]

Specifications

[edit]

Data from Jane's all the World's Aircraft 1931[3][4]

General characteristics

  • Crew: 1
  • Capacity: 6 pax
  • Length: 10 m (32 ft 10 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Height: 3.4 m (11 ft 2 in)
  • Wing area: 34 m2 (370 sq ft)
  • Empty weight: 1,167 kg (2,573 lb)
  • Gross weight: 2,050 kg (4,519 lb)
  • Fuel capacity: 276 kg (608 lb)
  • Powerplant: 3 × Renard Type 120 5-cylinder air-cooled radial piston engines, 89 kW (120 hp) each at 1,750 rpm; 100 kW (140 hp) at 1900 rpm for take-off
  • Propellers: 2-bladed wooden fixed-pitch propellers, 2.3 m (7 ft 7 in) diameter

Performance

  • Maximum speed: 207 km/h (129 mph, 112 kn)
  • Stall speed: 95 km/h (59 mph, 51 kn)
  • Range: 700 km (430 mi, 380 nmi)
  • Service ceiling: 6,100 m (20,000 ft)
  • Rate of climb: 4.4 m/s (870 ft/min)
  • Time to altitude: 2,000 m (6,600 ft) in 3 minutes
  • Wing loading: 60.4 kg/m2 (12.4 lb/sq ft)
  • Power/mass: 12.5 lb/hp (7.6 kg/kW)

References

[edit]
  1. ^ Taylor 1989, p.758
  2. ^ a b c d e f "Renard R-30". Fonds National Alfred Renard. Retrieved 2009-01-26.
  3. ^ Grey, C.G., ed. (1931). Jane's all the World's Aircraft 1931. London: Sampson Low, Marston & company, ltd. p. 6c.
  4. ^ "Trimoteur R-30". Fonds National Alfred Renard. Retrieved 2009-01-26.

Further reading

[edit]
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.