Editing Lockheed C-5 Galaxy (section)

==Specifications (C-5M)==
[[File:Lockheed C-5 Galaxy 3-view line drawing.jpg|thumb|Drawing lines]]
[[File:C5 Galaxy nose.jpg|thumb|A detail of the C-5's nose assembly raised for loading and unloading]]
[[File:USAF C-5 Galaxy Engine.jpg|thumb|A [[General Electric TF39]] turbofan engine]]
[[File:A CH-47F Chinook helicopter is unloaded from a C-5M Super Galaxy.jpg|thumb|Unloading one of two [[CH-47 Chinook|Chinook]] helicopters from a C-5M ''Super Galaxy'']]

{{Aircraft specs
|ref= Quest for Performance,<ref>Loftin, L.K., Jr. [http://www.hq.nasa.gov/pao/History/SP-468/cover.htm "NASA SP-468: Quest for Performance: The Evolution of Modern Aircraft."] {{Webarchive|url=https://web.archive.org/web/20060613210139/http://www.hq.nasa.gov/pao/History/SP-468/cover.htm |date=13 June 2006 }} ''NASA'', 1985.</ref> International Directory of Military Aircraft,<ref>Frawley, Gerald. ''The International Directory of Military Aircraft, 2002/2003''. Fishwick, Act, Australia: Aerospace Publications, 2002. {{ISBN|1-875671-55-2}}.</ref> and USAF fact sheet<ref name=USAF_fact_sht>[https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104492/c-5-abc-galaxy-c-5m-super-galaxy/ "C-5 A/B/C Galaxy and C-5M Super Galaxy fact sheet."] ''US Air Force'', January 2014. Retrieved 29 January 2014.</ref>
|prime units?=kts
<!--   General characteristics
-->
|crew=<br/>
** 7 typical (Aircraft Commander, First Pilot, 2 Flight Engineers, 3 Loadmasters);
** 4 minimum (pilot, copilot, two flight engineers){{#tag:ref|Loadmasters are not needed when flying without cargo.<ref name=AFMAN/>|group=N}}
** 8 when augmented (Aircraft Commander, 2 First Pilots, 2 Flight Engineers, 3 Loadmasters)<ref name=AFMAN>{{cite book |url=https://static.e-publishing.af.mil/production/1/af_a3/publication/afman11-2c-5v3/afman11-2c-5v3.pdf |title=AIR FORCE MANUAL 11-2C-5, VOLUME 3 |page=11 |date=20 October 2022}}</ref>
|capacity=<br/>
** 36 master pallets [[463L master pallet|463L]], {{cvt|281000|lb|0}}<ref name="af.mil fact sheet">{{Cite web|url=https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104492/c-5m-super-galaxy/|title=C-5M Super Galaxy|website=U.S. Air Force}}</ref>
|length ft=247
|length in=1
|length note=
|span ft=222
|span in=9
|span note=
|height ft=65
|height in=1
|height note=
|wing area sqft=6200
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil|NACA 0012.41 mod]]; '''tip:''' [[NACA airfoil|NACA 0011 mod]]<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=380000
|empty weight note=
|gross weight lb=<!-- 555000 Not sure where this value comes from. -->
|gross weight note=
|max takeoff weight lb=840000
|max takeoff weight note=<ref group=N>Exceeds normal recommended peacetime max takeoff weight.{{citation needed|date=October 2016}}</ref>
|fuel capacity= 341,446 lb (154,880 kg); {{cvt|51150|USgal|impgal L}}
|more general=
<!--   Powerplant
-->
|eng1 number=4
|eng1 name=[[General Electric CF6-80C2|General Electric F138-100]]
|eng1 type=[[turbofan]] engines
|eng1 lbf=51000
|eng1 note=
<!--   Performance
-->
|max speed kts=462
|max speed note=
|max speed mach=0.79
|cruise speed kts=450
|cruise speed note= / Mach 0.77<!--based on official speed 518 mph, and Mach 0.77 as normal cruise speed, it represents -50&nbsp;°C surrounding temperature, sonic speed is 1,082&nbsp;km/h-->
|stall speed kts=
|stall speed note=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kts=
|minimum control speed note=
|range nmi=4800
|range note= with a {{cvt|120000|lb|kg|0}} payload, {{cvt|2300|nmi|0}} at maximum cargo capacity<ref name="af.mil fact sheet" />
|combat range nmi=
|combat range note=
|ferry range nmi=7000
|ferry range note=with no cargo on board.
|endurance=<!-- if range unknown -->
|ceiling ft=41000
|ceiling note=at {{cvt|750000|lb|kg|0}}
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ftmin=2100
|climb rate note=
|time to altitude=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=0.26

|more performance=<br/>
*'''Take-off run:''' {{cvt|5400|ft}}
*'''Landing run:''' {{cvt|3600|ft}}
|avionics=
}}