Kolb Slingshot

Source: Wikipedia, the free encyclopedia.

Kolb Slingshot
Role
Ultralight aircraft
National origin United States
Manufacturer
New Kolb Aircraft
Status Production completed (2014)

The Kolb Slingshot is an American tandem two seat, high wing,

New Kolb Aircraft of London, Kentucky and intended for amateur construction.[1][2][3]

By mid-2014, the company was no longer offering the model for sale and production had ended.[4]

Design and development

The Slingshot was designed as a two-seat ultralight with a small wing and high cruise speed for the installed power, capable of delivering speeds comparable to a general aviation aircraft without the associated cost or complexity. The standard engine was originally the 64 hp (48 kW)

Rotax 912UL and 80 hp (60 kW) or 2si twin engine packs have been installed. In its home country the aircraft is normally licensed in the Experimental - amateur-built category.[1][2][3]

The design features a forward

aircraft fabric. The wings and horizontal tail are quick-folding for storage and ground transport. The Slingshot can be made ready to fly from trailering in 15 minutes.[1][2][3]

The long conventional landing gear consist of sprung tubing for the main gear, with a steerable sprung tailwheel.[2][3]

The company described the Slingshot's two seat capabilities, "the rear passenger seat is designed for average size people, up to 175 pounds. The seating arrangement has the passenger's legs overlapping the pilot's seat. This allows the fuselage to be shorter and more compact. It also saves a lot of weight.".[5]

Operational history

In reviewing the aircraft Andre Cliche said:

This tandem two-seater is a really hot little racer with a short speedwing and an oversized engine.[2]

Specifications (Slingshot)

Data from Kitplanes, Cliche and Purdy[1][2][3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 19 ft 0 in (5.79 m)
  • Wingspan: 22 ft 0 in (6.71 m)
  • Height: 6 ft 9 in (2.06 m)
  • Wing area: 110 sq ft (10 m2)
  • Empty weight: 345 lb (156 kg)
  • Gross weight: 850 lb (386 kg)
  • Fuel capacity: 10 US gallons (38 litres)
  • Powerplant: 1 ×
    two-stroke
    aircraft engine, 64 hp (48 kW)

Performance

  • Maximum speed: 100 mph (160 km/h, 87 kn)
  • Cruise speed: 87 mph (140 km/h, 76 kn)
  • Stall speed: 39 mph (63 km/h, 34 kn)
  • Never exceed speed: 125 mph (201 km/h, 109 kn)
  • g limits: +4/-2
  • Rate of climb: 1,300 ft/min (6.6 m/s)

Avionics

  • none

See also

Aircraft of comparable role, configuration, and era

References

  1. ^ a b c d Downey, Julia: 1999 Kit Aircraft Directory, Kitplanes, Volume 15, Number 12, December 1998, page 54. Primedia Publications. ISSN 0891-1851
  2. ^
    ISBN 0-9680628-1-4
  3. ^
    ISBN 0-9636409-4-1
  4. New Kolb Aircraft. "Kolb Aircraft Company". kolbaircraft.com. Archived from the original
    on January 4, 2014. Retrieved February 19, 2020.
  5. ^ "Kolb Aircraft Slingshot Experimental Light Kit Build Aircraft". Kolbaircraft.com. Archived from the original on September 11, 2012. Retrieved September 9, 2012.
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