Tupolev Tu-123

Tupolev Tu-123

__NOTOC__ Infobox Aircraft
name=Tu-123 Yastreb


caption=
type=Reconnaissance Drone
national origin=Soviet Union
manufacturer=Tupolev
designer=
first flight=
introduced=
retired=
status=
primary user=
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produced=
number built=
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The Tupolev Tu-123 Yastreb (Falcon, _ru. Ястреб) was one of the earliest Soviet reconnaissance drones that began development in 1960. Sometimes referred to as the "DBR-1", it was introduced in 1964.

The Tu-123 was a long-range, high-altitude supersonic strategic reconnaissance aircraft, in the form of a big dart, conceptually somewhat similar to the United States' D-21. It carried both film cameras and SIGINT payloads. The Tu-123 was ground-launched with RATO booster and powered by a KR-15 afterburning turbojet in flight. The Tu-123 was expendable, parachuting its payload to the ground for recovery. The KR-15 was an expendable version of the R-15 engine used on the twin-engine MiG-25 Foxbat interceptor. The lack of recovery capability was unsatisfactory. This concern led to the Tu-139 Yastreb 2, which could land on unprepared airstrips, but it was never put into production, since by that time the Soviets had shifted their emphasis to low-level reconnaissance.

pecifications

aerospecs
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met or eng?= met

crew=None
capacity=
length m=27.84
length ft=91
length in=4
span m=8.41
span ft=27
span in=7
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
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dia m=
dia ft=
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width m=
width ft=
width in=
height m=4.78
height ft=15
height in=8
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=11,450
empty weight lb=25,250
gross weight kg=35,610
gross weight lb=78,520
lift kg=
lift lb=

eng1 number=1
eng1 type=Tumansky KR-15
eng1 kw=
eng1 hp=
eng1 kn= 98.1
eng1 lbf= 22,046
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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max speed kmh=2,700
max speed mph=1,675
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=3,200
range miles=2,000
endurance h=
endurance min=
ceiling m=22,800
ceiling ft=74,800
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

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References

This article contains material that originally came from the web article [http://www.vectorsite.net/twuav.html "Unmanned Aerial Vehicles"] by Greg Goebel, which exists in the Public Domain.


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