- RQ-15 Neptune
__NOTOC__ Infobox Aircraft
name=RQ-15 Neptune
caption=
type=Maritime reconnaissance UAV
national origin=United States
manufacturer=DRS
designer=
first flight=January avyear|2002
introduced=
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primary user=United States Navy
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variants with their own articles=The DRS RQ-15 Neptune is a reconnaissanceUAV developed in the United States in the early years of the 21st century. The design is optimised for operations over water, and is capable of water landings on its flying-boat-like hull. The 11.2 kW (15 hp) pusher engine is mounted high to keep it dry during takeoffs and landings. The Neptune can also be launched off a pneumatic catapult and land on a skid.pecifications
aerospecs
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met or eng?= engcrew=None
capacity=20 lb (9 kg) payload
length m=1.83
length ft=6
length in=0
span m=2.13
span ft=7
span in=0
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empty weight kg=
empty weight lb=
gross weight kg=36
gross weight lb=80
lift kg=
lift lb=eng1 number=1
eng1 type=piston engine
eng1 kw= 11
eng1 hp= 15
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eng2 lbf-ab=max speed kmh=160
max speed mph=100
max speed mach=
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endurance h= 4
endurance min=
ceiling m=2,400
ceiling ft=8,000
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lists=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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* [http://www.drs.com/Products/NEPTUNE.aspx?cat=Intel_Tech&subcat=Sub_Cat_22 Manufacturer's website]
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