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Grumman E-2 Hawkeye
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==Specifications (E-2C)== [[File:Grumman E-2C Hawkeye 0014.svg|right|300px]] {{Aircraft specs |ref=US Navy fact file<ref>{{cite web|url=http://www.navy.mil/navydata/fact_display.asp?cid=1100&tid=700&ct=1|title=The US Navy β Fact File: E-2 Hawkeye early warning and control aircraft|first=Dan|last=Petty|work=navy.mil|access-date=August 1, 2016|archive-url=https://web.archive.org/web/20161019025728/http://www.navy.mil/navydata/fact_display.asp?cid=1100&tid=700&ct=1|archive-date=October 19, 2016|url-status=dead}}</ref> E-2D Storybook (page 25)<ref>{{cite web|url=http://www.northropgrumman.com/Capabilities/E2CHawkeye2000/Documents/pageDocuments/E-2D_Storybook.pdf|title=E-2D_Storybook|work=northropgrumman.com|access-date=August 1, 2016|archive-url=https://web.archive.org/web/20160303222855/http://www.northropgrumman.com/Capabilities/E2CHawkeye2000/Documents/pageDocuments/E-2D_Storybook.pdf|archive-date=March 3, 2016|url-status=live}}</ref> |prime units?=kts <!-- General characteristics --> |crew=5: pilot, copilot, radar officer (RO), combat information center officer (CICO), aircraft control officer (ACO) |length ft=57 |length in=8+3/4 |length note= |span ft=80 |span in=7 |span note= |height ft=18 |height in=3+3/4 |height note= : Radome could retract by {{convert|2|ft|m|1}} to fit into the {{cvt|17|ft|6|in|m}} clear height hangar of Essex and Midway class carriers. Retraction function no longer used. |wing area sqft=700 |wing area note=<ref name="JAWA03 p688-9">Jackson 2003, pp. 688β689.</ref> |aspect ratio=9.15 |airfoil='''root:''' [[NACA airfoil|NACA 63A216]]; '''tip:''' [[NACA airfoil|NACA 63A414]]<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 |archive-url=https://web.archive.org/web/20190326174850/https://m-selig.ae.illinois.edu/ads/aircraft.html |archive-date=March 26, 2019 |url-status=live}}</ref> |empty weight lb=40200 |empty weight note= |gross weight lb=43068 |gross weight note= |max takeoff weight lb=57500 |max takeoff weight note= |fuel capacity= |more general= <!-- Powerplant --> |eng1 number=2 |eng1 name=[[Allison/Rolls-Royce T56-A-427]] (E-2C), T56-A-427A (E-2D) |eng1 type=turboprop |eng1 shp=5100 |eng1 note= |prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |max speed kts=350 |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kts=256 |cruise speed note= |stall speed kts= |stall speed note= |never exceed speed kts= |never exceed speed note= |minimum control speed kts= |minimum control speed note= |range nmi= |range note= |combat range nmi= |combat range note= |ferry range nmi=1462 |ferry range note= |endurance=6 hours (8 hours land-based)<ref>{{cite web |last1=Gady |first1=Franz-Stefan |title=Japan Takes Delivery of First E-2D Advanced Hawkeye Aircraft |url=https://thediplomat.com/2019/06/japan-takes-delivery-of-first-e-2d-advanced-hawkeye-aircraft/ |website=thediplomat.com |publisher=The Diplomat |access-date=5 June 2019 |archive-url=https://web.archive.org/web/20190603201337/https://thediplomat.com/2019/06/japan-takes-delivery-of-first-e-2d-advanced-hawkeye-aircraft/ |archive-date=June 3, 2019 |url-status=live}}</ref> |ceiling ft=34700 |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ftmin= |climb rate note= |time to altitude= |wing loading lb/sqft=72.7 |wing loading note= |fuel consumption lb/mi= |power/mass={{cvt|0.19|hp/lb}} |more performance= |avionics= *AN/APS-145 Radar *OL-483/AP IFF interrogator system *APX-100 IFF Transponder *OL-698/ASQ Tactical Computer Group *AN/ARC-182 UHF/VHF radio *AN/ARC-158 UHF radio *AN/ARQ-34 HF radio *AN/USC-42 Mini-DAMA SATCOM system }}
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