Rahul Sharma (Editor)

US Aviation Cumulus

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
First flight
  
1995

Manufacturer
  
US Aviation

US Aviation Cumulus httpswwwpilotmixcomimagesacimagescumulus2jpg

The US Aviation Cumulus is an American low-wing, single-seat, open cockpit motor glider that was designed by Dave Ekstrom and produced by US Aviation, supplied in kit form for amateur construction.

Contents

Design and development

The Cumulus was conceived as a lightweight motorglider for soaring and also for touring. It is a development of the earlier US Aviation Cloud Dancer design. The aircraft production was outsourced, initially produced by AeroDreams it was later produced by Dave Ekstrom for US Aviation after 2004. The Cumulus first flew in 1995 and was named after the cumulus cloud.

Built from steel tubing, composites and fabric, the Cumulus is powered by a standard Rotax 447 40 hp (30 kW) engine in pusher configuration, although engines from 20 to 55 hp (15 to 41 kW) can be fitted. The wings are detachable for transport or storage. It has a glide ratio of 20:1. The landing gear is conventional and the cruciform tail is strut-braced.

Construction time from the kit is estimated at 200 hours.

Specifications (Cumulus)

Data from Purdy and KitPlanes

General characteristics

  • Length: 20 ft 0 in (6.10 m)
  • Wingspan: 43 ft 0 in (13.11 m)
  • Height: 4 ft 6 in (1.37 m)
  • Wing area: 141 sq ft (13.1 m2)
  • Aspect ratio: 13:1
  • Empty weight: 320 lb (145 kg)
  • Gross weight: 560 lb (254 kg)
  • Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  • Powerplant: 1 × Rotax 447 twin cylinder, two-stroke iarcraft engine, 40 hp (30 kW)
  • Performance

  • Maximum speed: 85 mph (137 km/h; 74 kn)
  • Cruise speed: 75 mph (121 km/h; 65 kn)
  • Stall speed: 32 mph (51 km/h; 28 kn) in landing configuration
  • Never exceed speed: 89 mph; 78 kn (144 km/h)
  • Range: 275 mi (239 nmi; 443 km)
  • Service ceiling: 15,000 ft (4,600 m)
  • Maximum glide ratio: 20:1 at 34 mph (55 km/h)
  • Rate of climb: 800 ft/min (4.1 m/s)
  • Rate of sink: 195 ft/min (0.99 m/s) at 43 mph (69 km/h)
  • References

    US Aviation Cumulus Wikipedia


    Similar Topics