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General Atomics MQ-1 Predator
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==Specifications== [[File:USAF RQ-1B Predator UAV 3view.jpg|thumb|RQ-1B Predator 3-view drawing]] [[File:MQ-1B 3view.jpg|thumb|MQ-1B Predator 3-view drawing]] {{Aircraft specs |ref= USAF MQ-1B fact sheet<ref name="factsheet" /> |prime units?=kts <!-- General characteristics --> |crew=0, 3 on ground out of theater, (remote pilot, sensor operator, and intelligence analyst), with in-theater ground handling crew |capacity= |length ft=27 |length in=0 |span m=14.8 |span note= ::::'''MQ-1B Block 10/15:''' {{cvt|16.84|m|order=flip}}<ref name="Factsheets : MQ-1B Predator"/> |height m=2.1 |wing area sqft=123.3 |wing area note=<ref name="warfighterpedia" /> |aspect ratio=19 |airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref>--> |empty weight lb=1130 |empty weight note= |gross weight kg=1020 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity=851 lb (387 kg) |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=[[Rotax 914F]] |eng1 type=4-cylinder air-cooled turbocharged horizontally-opposed piston engine |eng1 hp=115 |prop blade number=2 |prop name=constant-speed pusher propeller |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |max speed kts=117 |max speed note= |cruise speed kts=70 |cruise speed note= to {{cvt|90|kn|mph km/h}} |stall speed kts=54 |stall speed note= |never exceed speed kts= |never exceed speed note= |minimum control speed kts= |minimum control speed note= |range nmi=675 |range note= |combat range nmi= |combat range note= |ferry range nmi= |ferry range note= |endurance=24 hours<ref name="deagel.com" /> |ceiling ft=25000 |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ftmin=<!-- sailplanes --> |sink rate note= |lift to drag= |wing loading lb/sqft= |wing loading note= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance= <!-- Armament --> |hardpoints=2 |hardpoint missiles=<br/> *** 2 Γ [[AGM-114 Hellfire]] (MQ-1B) *** 4 Γ [[Air-to-Air Stinger (ATAS)]] (MQ-1B) *** 6 Γ [[AGM-176 Griffin]] air-to-surface missiles<ref name="Small Raytheon Missile Deployed on Predator" /> |avionics=* ASIP-1C * AN/AAS-52 Multi-Spectral Targeting System * AN/ZPQ-1 [[synthetic-aperture radar]] (early airframes only) }}
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