Gulfstream American Peregrine

__NOTOC__ Infobox Aircraft
name=Peregrine 600


caption=
type=Military trainer
national origin=United States of America
manufacturer=Gulfstream American
designer=
first flight=22 May avyear|1981
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Gulfstream American Peregrine 600 was a military trainer aircraft developed in the United States in the early 1980s but which did not progress further than prototype stage. Developed from the company's Hustler business aircraft, the Peregrine shared the same wings, empennage and rear fuselage, but had a new forward fuselage with side-by-side seating for the pilot and instructor. The aircraft was developed as a contender in the United States Air Force's Next Generation Trainer programme, but was ultimately passed over in favour of the Fairchild T-46. Attempts to market it to (at least) the air forces of Australia, New Zealand, Japan, and China also proved unsuccessful, and the project was cancelled in 1985.

pecifications

aerospecs
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met or eng?= eng

crew=Two, pilot and instructor
capacity=
length m=11.70
length ft=38
length in=4
span m=10.50
span ft=34
span in=5
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=4.10
height ft=13
height in=5
wing area sqm=
wing area sqft=
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=2,800
gross weight lb=6,200
lift kg=
lift lb=

eng1 number=1
eng1 type=Pratt & Whitney JT15D
eng1 kw=
eng1 hp=
eng1 kn=
eng1 lbf=
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eng2 number=
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max speed kmh=730
max speed mph=450
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=2,000
range miles=1,240
endurance h=
endurance min=
ceiling m=14,600
ceiling ft=48,000
glide ratio=
climb rate ms=26.4
climb rate ftmin=5,200
sink rate ms=
sink rate ftmin=

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References

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