- IAI Nammer
__NOTOC__ Infobox Aircraft
name=Nammer
caption=
type=Fighter
national origin=Israel
manufacturer=IAI
designer=
first flight=21 March avyear|1991
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The IAI "Nammer" (נמר "Leopard", but frequently mistranslated "Tiger") was a fighter aircraft developed in Israel in the late 1980s and early 1990s as a modernised version of the Kfir for the export market. Although a prototype was built and flown, buyers were not forthcoming and development was ceased without any further examples being constructed. The avionics of the Nammer were to have taken advantage of the work undertaken for the cancelled Lavi project.As initially announced, the Nammer was to be an upgrade package for existing Mirage III and Mirage 5 airframes. Customers would be offered a choice of two configurations, one based around re-engining the aircraft with a
General Electric F404 , the other around retaining the Mirage'sSNECMA Atar engine but integrating theElta EL/M-2011 or EL/M-2032 fire-control radar. The first of these options maximised performance and range, the second maximised the aircraft's air-to-air targeting capabilities. As development progressed, the Nammer came to be advertised as a new-build aircraft with the EL/M-2032 an integral part of the package, and customers able to choose their preferred engine out of the F404 (or its Volvo derivative, the RM-12), theSNECMA M53 , or thePratt & Whitney PW1120 . The design strongly resembled the Kfir C-7,but was easily distinguished by its longer nose and lack of a dorsal air scoop under the tail fin. The asking price was $US 20 million, and IAI stated that it would not commence production without orders for 80 aircraft.pecifications (as designed)
aerospecs
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met or eng?= metcrew=One pilot
capacity=
length m=16.00
length ft=52
length in=6
span m=8.22
span ft=27
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
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width m=
width ft=
width in=
height m=4.55
height ft=14
height in=11
wing area sqm=34.8
wing area sqft=375
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=16,511
gross weight lb=36,400
lift kg=
lift lb=eng1 number=1
eng1 type=various
eng1 kw=
eng1 hp=
eng1 kn= 80-90
eng1 lbf= 18,000-20,000
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=
max speed mph=
max speed mach= 2.2
cruise speed kmh=
cruise speed mph=
range km=1,382
range miles=859
endurance h=
endurance min=
ceiling m=17,700
ceiling ft=58,000
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=2 × fixed, forward-firing 30 mm
DEFA cannon s
armament2=6,270 kg (13,790 lb) of external stores
armament3=
armament4=
armament5=
armament6= aircontent
see also=
related=
similar aircraft=
lists=References
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