Editing Lockheed C-130 Hercules (section)

==Specifications (C-130H)==
[[File:Lockheed C-130H Hercules Line Drawing.svg|thumb]]
[[File:C-130 Hercules cockpit hg.jpg|thumb|C-130H Hercules flight deck]]
[[File:C-130 Hercules 10.jpg|thumb|A Hercules deploying flares, sometimes referred to as ''Angel Flares'' due to the characteristic pattern]]
[[File:Lockheed Hercules interior.jpg|thumb|Cargo compartment of a Swedish Air Force C-130]]

{{Aircraft specs
|ref= USAF C-130 Hercules fact sheet,<ref name="airforcefactsheet">{{cite web |title=C-130 Hercules |url=https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104517/c-130-hercules/ |year=2003 |edition=May 2014 |publisher= United States Air Force |archive-url=https://web.archive.org/web/20140914210641/http://www.af.mil/AboutUs/FactSheets/Display/tabid/224/Article/104517/c-130-hercules.aspx |archive-date=14 September 2014 |url-status=live}}</ref> ''International Directory of Military Aircraft'',<ref name="Frawley Military">Frawley 2002, p. 108.</ref> ''Complete Encyclopedia of World Aircraft'',<ref name= Donald>Donald 1997</ref> and ''Encyclopedia of Modern Military Aircraft''.<ref name=Eden>Eden 2004</ref>
|prime units?=kts
<!--   General characteristics
-->
|crew=5 (2 pilots, [[CSO/navigator]], [[flight engineer]] and [[loadmaster]])
|capacity={{cvt|42000|lb}} payload
** C-130E/H/J cargo hold: length, {{convert|40|ft|m|2|abbr=on}}; width, {{convert|9|ft|11|in|m|2|abbr=on}}; height, {{convert|9|ft|m|2|abbr=on}}. Rear ramp: length, {{convert|123|in|m|2|abbr=on}}; width, {{convert|119|in|m|2|abbr=on}}
** C-130J-30 cargo hold: length, {{convert|55|ft|m|2|abbr=on}}; width, {{convert|9|ft|11|in|m|2|abbr=on}}; height, {{convert|9|ft|m|2|abbr=on}}. Rear ramp: length, {{convert|123|in|m|2}}; width, {{convert|119|in|m|2|abbr=on}}
** 92 [[passengers]] ''or''
** 64 [[airborne troops]] ''or''
** 74 litter patients with 5 medical crew ''or''
** 6 pallets ''or''
** 2–3 [[Humvee]]s ''or''
** 2 [[M113 armored personnel carrier]]s
** 1 [[CAESAR self-propelled howitzer]]
|length ft=97
|length in=9
|length note=
|span ft=132
|span in=7
|span note=
|height ft=38
|height in=3
|height note=
|wing area sqft=1745
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 64A318]]; '''tip:''' [[NACA airfoil|NACA 64A412]]<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 |publisher=UIUC Applied Aerodynamics Group, University of Illinois |date=15 September 2010|access-date=16 April 2019 |archive-url= https://web.archive.org/web/20190326174850/https://m-selig.ae.illinois.edu/ads/aircraft.html |archive-date=26 March 2019 |url-status=live}}</ref>
|empty weight lb=75800
|empty weight note=
|gross weight lb=
|gross weight note=
|max takeoff weight lb=155000
|max takeoff weight note=
|fuel capacity=
|more general=
<!--   Powerplant
-->
|eng1 number=4
|eng1 name=[[Allison T56]]-A-15
|eng1 type=[[turboprop]] engines
|eng1 kw=<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng1 shp=4590

|prop blade number=4
|prop name=[[Hamilton Standard]] 54H60 constant-speed fully feathering reversible propellers
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=13
|prop dia in=6
|prop dia note=<ref name="Lockheed Service News">{{Cite journal |title=The 54H60 Propeller |journal=Lockheed Martin Service News |year=1999 |last=Webb |first=L. R. |volume=26 |issue=3 |pages=4–5 |access-date=13 August 2019 |url=https://www.lockheedmartin.com/content/dam/lockheed-martin/aero/documents/sustainment/csc/service-news/sn-mag-v21-v30/v26n3.pdf |archive-url=https://web.archive.org/web/20190813224721/https://www.lockheedmartin.com/content/dam/lockheed-martin/aero/documents/sustainment/csc/service-news/sn-mag-v21-v30/v26n3.pdf |archive-date=2019-08-13 |url-status=live}}</ref>
<!--   Performance
-->
|max speed kts=320
|max speed note=at {{cvt|20000|ft}}
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kts=292
|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=2050
|range note=
|combat range nmi=
|combat range note=
|ferry range nmi=3995
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling ft=33000
|ceiling note= empty<ref name="aerospceweb">{{cite web |title=Lockheed C-130 Hercules Heavy Transport |url=http://www.aerospaceweb.org/aircraft/transport-m/c130/ |publisher=aerospaceweb.org |access-date=29 May 2019 |archive-url=https://web.archive.org/web/20190109145041/http://www.aerospaceweb.org/aircraft/transport-m/c130/ |archive-date=9 January 2019 |url-status=live}}</ref>
::::{{cvt|23000|ft}} with&nbsp;{{cvt|42000|lb}} payload
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ftmin=1830
|climb rate note=
|time to altitude=
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading lb/sqft=
|wing loading note=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=

|more performance=*'''Takeoff distance:''' {{cvt|3586|ft|0}} at {{cvt|155000|lb|0}} max gross weight;<ref name=Eden/>
::::{{cvt|1400|ft|0}} at {{cvt|80000|lb|0}} gross weight<ref name="uscost.netarchived">{{cite web |title=Aircraft Characteristics: C-130 Hercules |url=http://www.uscost.net/aircraftcharacteristics/acc130.htm |publisher=uscost.net |access-date=29 May 2019 |archive-url=https://web.archive.org/web/20090727104754/http://www.uscost.net/aircraftcharacteristics/acc130.htm |archive-date=27 July 2009}}</ref>
|avionics=
* [[Westinghouse Electric (1886)|Westinghouse Electronic Systems]] [[List of radars#AN/APN Series|AN/APN-241 weather and navigational radar]]<ref name="elecsyssect">{{cite web |title=AN/APN-241 Color Weather/Navigation Radar with Prediction Windshear Detection |url=http://www.es.northropgrumman.com/solutions/apn241/index.html |publisher=Electronic systems sector, Northrop Grumman |access-date=29 May 2019 |archive-url=https://web.archive.org/web/20080321234418/http://www.es.northropgrumman.com/solutions/apn241/index.html |archive-date=21 March 2008}}</ref>
}}