- Bowers Namu II
__NOTOC__ Infobox Aircraft
name=Namu II
caption=
type=Recreational aircraft
manufacturer=Homebuilt
designer=Peter Bowers
first flight=
introduced=
retired=
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number built=4
variants with their own articles=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 andBoeing historianPeter Bowers .Development
The aircraft was a follow-on project to the designer's earlier
Bowers Fly Baby design, if considerably larger; a low-wingcantilever monoplane with an invertedgull 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, theorca captive in Bower's home city ofSeattle , 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.
pecifications
aerospecs
met or eng?= engcrew=one pilot
capacity=1 passenger
length m=6.55
length ft=21
length in=6
span m=10.06
span ft=33
span in=0
dia m=
dia ft=
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height m=
height ft=
height in=
wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=
gross weight lb=eng1 number=1
eng1 type=Lycoming O-290 Gflat-four engine
eng1 kw= 93
eng1 hp= 125
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=217
max speed mph=135
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=800
range miles=500
endurance h=
endurance min=
ceiling m=4,580
ceiling ft=15,000
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
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armament6=References
*
* "Pete Bowers" "Wind in the Wires" Vol XIV No 10
* [http://www.aerofiles.com/_bo.html aerofiles.com]ee also
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