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Aerodyne Systems Vector

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(Redirected fromAerodyne Systems Vector 600)
American ultralight aircraft

Vector
Aerodyne Vector 610 atFlyhistorisk Museum, Sola
General information
TypeUltralight aircraft
National originUnited States
ManufacturerAerodyne Systems
StatusProduction completed
History
Introduction date1982
Developed fromHill Humbug
VariantUltralight Flight Mirage

TheAerodyne Systems Vector is a family ofAmericanultralight aircraft that was designed by Berndt Petterson, Mike McCarron and Paul Yarnell and produced byAerodyne Systems, introduced in 1982. The aircraft was supplied as a kit foramateur construction.[1][2]

Design and development

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The Vector owes many of its design concepts to the earlierHill Humbug and was later to inspire and influence theUltralight Flight Mirage.[1][2]

The Vector was designed to comply with the USFAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 195 lb (88 kg). It features acable-bracedhigh-wing,V-tail, a single-seat, open cockpit,tricycle landing gear and a single engine inpusher configuration.[1][2]

The aircraft is made from bolted-togetheraluminum tubing, with its flying surfaces covered inDacron sailcloth. Its 80% double-surface 35.2 ft (10.7 m) span wing is supported by cables running from an inverted "V"kingpost. Thelanding gear's nose wheel is not steerable and a small tail caster is provided. The pilot is accommodated on an open seat, without a windshield. The engine is mounted at the wing'sleading edge and powers thetrailing edge-mounted pusher propeller through an extension shaft.[1][2]

The Vector series was very popular in its day and a great number were produced.[1]

Variants

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Vector 600
Initial model, with a two-axis control system, powered by two 9 hp (7 kW)Chrysler engines.[1]
Vector 610
Improved model, with a structurally strengthenedairframe, enlargedspoilers, ellipticalwing tip extensions and powered by a single 22 hp (16 kW)Zenoah G-25B single cylinder,two-stroke engine.[1]
Vector 627
Powered by a single 28 hp (21 kW) single cylinder, two-strokeRotax 277 engine.[1]
Vector 627 SR
Powered by a single 35 hp (26 kW) single cylinder, two-strokeRotax 377 engine.[1]

Specifications (Vector 610)

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Data from Cliche and the Virtual Ultralight Museum[1][2]

General characteristics

  • Crew: one
  • Length: 18 ft (5.5 m)
  • Wingspan: 35.2 ft (10.7 m)
  • Height: 8 ft (2.4 m)
  • Wing area: 154 sq ft (14.3 m2)
  • Empty weight: 195 lb (88 kg)
  • Gross weight: 445 lb (202 kg)
  • Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  • Powerplant: 1 ×Zenoah G-25B single cylinder,two-stroke aircraft engine, 22 hp (16 kW)

Performance

  • Cruise speed: 45 mph (72 km/h, 39 kn)
  • Stall speed: 26 mph (42 km/h, 23 kn)
  • Range: 125 mi (201 km, 109 nmi)
  • g limits: +5.7/-2.8
  • Rate of climb: 600 ft/min (3.0 m/s)

References

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  1. ^abcdefghijCliche, Andre:Ultralight Aircraft Shopper's Guide 8th Edition, page E-42. Cybair Limited Publishing, 2001.ISBN 0-9680628-1-4
  2. ^abcdeVirtual Ultralight Museum (n.d.)."Vector 600". Retrieved3 January 2012.

External links

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Wikimedia Commons has media related toAerodyne Vector.
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