- Bölkow Bo 103
__NOTOC__ Infobox Aircraft
name=Bo 103
caption=
type=Experimental helicopter
manufacturer=Bölkow
designer=
first flight=9 September 1961
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Bölkow Bo 103 was a small experimental helicopter flown in Germany in 1961 to research new rotor systems. While the mechanics of the aircraft were based on the Bo 102 captive training rig, the Bo 103 was capable of fully independent flight. In configuration, it was absolutely minimalist - consisting of nothing more than a tubular frame to which the dynamic components and the pilots seat were attached, although a small fibreglass cabin was eventually attached. The aircraft retained the Bo 102's single-rotor ofGlass-reinforced plastic , and proved that this was suitable for true flight. The prototype is preserved at theHubschraubermuseum Bückeburg .pecifications
aerospecs
met or eng?= metcrew=one pilot
capacity=
length m=
length ft=
length in=
span m=
span ft=
span in=
rot number= 1
rot dia m= 6.66
rot dia ft= 21
rot dia in= 10
height m=2.41
height ft=7
height in=11
wing area sqm=
wing area sqft=
rot area sqm= 34.8
rot area sqft= 374
aspect ratio=
empty weight kg=268
empty weight lb=591
gross weight kg=390
gross weight lb=860eng1 number=1
eng1 type=Agusta GA.70
eng1 kw= 61
eng1 hp= 82
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=100
max speed mph=60
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=100
range miles=60
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=5.7
climb rate ftmin=1,120
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=References
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* [http://www.eads.com/1024/en/eads/history/airhist/1960_1969/bo103_1961.html EADS website]ee also
aircontent
related=
similar aircraft=
sequence=
Bo 102 - Bo 103 - Bo 104 - Bo 105 - Bo 106 →lists=
see also=
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