To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Bowers Namu II

From Wikipedia, the free encyclopedia

Namu II
Role Recreational aircraft
Manufacturer Homebuilt
Designer Peter Bowers
First flight 2 July 1975
Number built 4

The Bowers Namu II was a single-engine, two-seat, recreational aircraft, designed and flown in the United States in the late 1970s and marketed for homebuilding. It was designed by famed aircraft designer and Boeing historian Peter Bowers.

Development

The aircraft was a follow-on project to the designer's earlier Bowers Fly Baby design, if considerably larger; a low-wing cantilever monoplane with an inverted gull wing and fixed tailwheel undercarriage, designed to carry two persons (the Fly Baby was a single-seat aircraft). The Namu II accommodated a passenger seated beside the pilot. The aircraft's somewhat portly lines provided the "Namu II" name, after Namu, the orca captive in Bower's home city of Seattle, Washington State.

Sales were disappointing, and out of the few plan sets sold, only four examples were constructed, one of which sported an orca paint job.

Operational history

In November 2022, there were no Namus remaining registered in the United States with the Federal Aviation Administration.[1]

Specifications

Data from Jane's All The World's Aircraft 1976–77[2]

General characteristics

  • Crew: one pilot
  • Capacity: 1 passenger
  • Length: 21 ft 6 in (6.55 m)
  • Wingspan: 33 ft 0 in (10.06 m)
  • Wing area: 150 sq ft (14 m2)
  • Airfoil: NACA 4415 root, NACA 4412 tip
  • Empty weight: 1,200 lb (544 kg)
  • Gross weight: 1,850 lb (839 kg)
  • Fuel capacity: 32 US gal (27 imp gal; 120 L)
  • Powerplant: 1 × Lycoming O-290G air-cooled flat-four engine , 125 hp (93 kW)

Performance

  • Maximum speed: 140 mph (230 km/h, 120 kn)
  • Cruise speed: 126 mph (203 km/h, 109 kn)
  • Range: 500 mi (800 km, 430 nmi)
  • Service ceiling: 15,000 ft (4,600 m)
  • Rate of climb: 950 ft/min (4.8 m/s)

References

  1. ^ Federal Aviation Administration (25 November 2022). "Make / Model Inquiry". Retrieved 25 November 2022.
  2. ^ Taylor 1976, p. 502.
  • Taylor, John W. R. (1976). Jane's All The World's Aircraft 1976–77. London: Jane's Yearbooks. ISBN 0-354-00538-3.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 194.
  • "Pete Bowers" Wind in the Wires Vol XIV No 10
  • aerofiles.com
This page was last edited on 25 November 2022, at 14:43
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.