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Robertson B1-RD

The Robertson B1-RD is an American ultralight aircraft that was designed by Glen Bashforth and Bruce Bashforth and produced by the Robertson Aircraft Corporation. The aircraft was supplied as a kit for amateur construction with production starting in June 1982.[1]

B1-RD
Role Ultralight aircraft
National origin United States
Manufacturer Robertson Aircraft Corporation
Designer Glen Bashforth and Bruce Bashforth
Introduction June 1982
Status Production completed
Produced June 1982-1984

Design and development edit

The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The B1-RD has a standard empty weight of 220 lb (100 kg). It has a cable-braced high-wing, single-seat, open cockpit, single engine in tractor engine configuration, and is equipped with conventional landing gear.[1]

The aircraft is made from bolted together aluminum tubing with the wings and tail surfaces covered in Dacron sailcloth. Its 32 ft (9.8 m) span wing is cable-braced to a top surface inverted "V" kingpost. The wing is a single-surface airfoil with a double-surface wing covering optional. The controls are conventional three-axis, including Junkers-style flaperons. The main fuselage structure is an aluminum keel tube that runs from the tail, mounts the wings and then the engine at the front. The original standard engines were the 30 hp (22 kW) Cuyuna 430R and the 20 hp (15 kW) Cuyuna 215. The landing gear has bungee-suspension on all three wheels and the tailwheel is steerable.[1]

Production of the B1-RD was curtailed circa 1984 due to liability concerns.[1]

Variants edit

In addition to the standard single-seat model, a two-seat version of the B1-RD was also marketed.[1]

Specifications (B1-RD) edit

Data from Cliche[1]

General characteristics

  • Crew: one
  • Wingspan: 32 ft 0 in (9.75 m)
  • Wing area: 162 sq ft (15.1 m2)
  • Empty weight: 220 lb (100 kg)
  • Gross weight: 500 lb (227 kg)
  • Fuel capacity: 4 U.S. gallons (15 L; 3.3 imp gal)
  • Powerplant: 1 × Cuyuna 430R two-cylinder, two-stroke aircraft engine, 30 hp (22 kW)

Performance

  • Maximum speed: 50 mph (80 km/h, 43 kn)
  • Cruise speed: 38 mph (61 km/h, 33 kn)
  • Stall speed: 15 mph (24 km/h, 13 kn)
  • Never exceed speed: 75 mph (121 km/h, 65 kn)
  • Range: 125 mi (201 km, 109 nmi)
  • Service ceiling: 14,000 ft (4,300 m)
  • g limits: +3/-2
  • Maximum glide ratio: 8.5:1
  • Rate of climb: 850 ft/min (4.3 m/s)
  • Rate of sink: 300 ft/min (1.5 m/s)

References edit

  1. ^ a b c d e f Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-4. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4

External links edit

  • Photo of B1-RD
  • Photo of B1-RD
  • Photo of B1-RD

robertson, american, ultralight, aircraft, that, designed, glen, bashforth, bruce, bashforth, produced, robertson, aircraft, corporation, aircraft, supplied, amateur, construction, with, production, starting, june, 1982, role, ultralight, aircraft, national, o. The Robertson B1 RD is an American ultralight aircraft that was designed by Glen Bashforth and Bruce Bashforth and produced by the Robertson Aircraft Corporation The aircraft was supplied as a kit for amateur construction with production starting in June 1982 1 B1 RD Role Ultralight aircraft National origin United States Manufacturer Robertson Aircraft Corporation Designer Glen Bashforth and Bruce Bashforth Introduction June 1982 Status Production completed Produced June 1982 1984 Contents 1 Design and development 2 Variants 3 Specifications B1 RD 4 References 5 External linksDesign and development editThe aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules including the category s maximum empty weight of 254 lb 115 kg The B1 RD has a standard empty weight of 220 lb 100 kg It has a cable braced high wing single seat open cockpit single engine in tractor engine configuration and is equipped with conventional landing gear 1 The aircraft is made from bolted together aluminum tubing with the wings and tail surfaces covered in Dacron sailcloth Its 32 ft 9 8 m span wing is cable braced to a top surface inverted V kingpost The wing is a single surface airfoil with a double surface wing covering optional The controls are conventional three axis including Junkers style flaperons The main fuselage structure is an aluminum keel tube that runs from the tail mounts the wings and then the engine at the front The original standard engines were the 30 hp 22 kW Cuyuna 430R and the 20 hp 15 kW Cuyuna 215 The landing gear has bungee suspension on all three wheels and the tailwheel is steerable 1 Production of the B1 RD was curtailed circa 1984 due to liability concerns 1 Variants editIn addition to the standard single seat model a two seat version of the B1 RD was also marketed 1 Specifications B1 RD editData from Cliche 1 General characteristicsCrew one Wingspan 32 ft 0 in 9 75 m Wing area 162 sq ft 15 1 m2 Empty weight 220 lb 100 kg Gross weight 500 lb 227 kg Fuel capacity 4 U S gallons 15 L 3 3 imp gal Powerplant 1 Cuyuna 430R two cylinder two stroke aircraft engine 30 hp 22 kW Performance Maximum speed 50 mph 80 km h 43 kn Cruise speed 38 mph 61 km h 33 kn Stall speed 15 mph 24 km h 13 kn Never exceed speed 75 mph 121 km h 65 kn Range 125 mi 201 km 109 nmi Service ceiling 14 000 ft 4 300 m g limits 3 2 Maximum glide ratio 8 5 1 Rate of climb 850 ft min 4 3 m s Rate of sink 300 ft min 1 5 m s References edit a b c d e f Cliche Andre Ultralight Aircraft Shopper s Guide 8th Edition page E 4 Cybair Limited Publishing 2001 ISBN 0 9680628 1 4External links editPhoto of B1 RD Photo of B1 RD Photo of B1 RD Retrieved from https en wikipedia org w index php title Robertson B1 RD amp oldid 1072675370, wikipedia, wiki, book, books, library,

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