Editing Airbus Beluga (section)

==Specifications (A300-600ST)==
[[File:Airbus A300 Beluga v1.0.png|350px|Layout of A300-600ST Beluga]]
{{Aircraft specs
| ref =Airbus,<ref name='abspecs'>{{Cite web |url= http://www.airbus.com/aircraftfamilies/freighter/beluga/specifications/ |title= Airbus Aircraft Family: Beluga – Dimensions & key data |publisher= Airbus |language = en-gb |url-status= dead |archive-url= https://web.archive.org/web/20140817213624/http://www.airbus.com/aircraftfamilies/freighter/beluga/specifications/ |archive-date= 17 August 2014 |df= dmy-all }}</ref> Airbus: Beluga<ref name="BelugaSTspecs">{{cite web |title=Beluga |url=https://www.airbus.com/aircraft/freighter/beluga.html#details |website=Airbus |access-date=16 September 2019 |language=en-gb}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=2<ref name=TCDS>{{cite web|title=Airbus A300-600ST Type Certificate Data Sheet|url=https://www.easa.europa.eu/system/files/dfu/EASA-TCDS-A.014_A300--600ST_Beluga-03-05052010.pdf|publisher=European Aviation Safety Agency|date=5 May 2010|access-date=11 October 2016|archive-date=22 January 2015|archive-url=https://web.archive.org/web/20150122170857/http://easa.europa.eu/system/files/dfu/EASA-TCDS-A.014_A300--600ST_Beluga-03-05052010.pdf|url-status=dead}}</ref>
|capacity={{cvt|47000|kg|0}} typical load
|length m=56.15
|length note=
|span m=44.84
|span note=
|height m=17.24
|height note=
|wing area sqm=260<ref name=elsevier>{{cite web |url= http://booksite.elsevier.com/9780340741528/appendices/data-a/table-1/table.htm |title= Airbus Aircraft Data File |publisher= Elsevier |work= Civil Jet Aircraft Design |date= July 1999}}</ref>
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg={{#expr:133500-47000}} <!--Maximum zero-fuel weight - capacity-->
|empty weight note=
|gross weight kg=
|gross weight note=
|max takeoff weight kg=155000
|max takeoff weight note=
|fuel capacity={{cvt|23860|L|USgal|0}}
| more general            =
*'''Fuselage external diameter:''' {{cvt|7.31|m|0}} (including lower fuselage)
* '''Cargo cross-section diameter:''' {{cvt|7.1|m|ftin}} in cargo compartment<ref name='freight'>{{Cite web |url=http://www.airbus.com/en/aircraftfamilies/beluga/freight |title=Beluga A300-600ST / Freight |publisher=Airbus |language = en-gb |access-date=10 May 2007 |archive-url=https://web.archive.org/web/20091102081716/http://www.airbus.com/en/aircraftfamilies/beluga/freight |archive-date=2 November 2009 |url-status=dead  }}</ref>
* '''[[Cargo hold]]''' – volume {{cvt|1500|m3}}, {{cvt|37.7|m}} long × {{cvt|7.04|m}} wide × {{cvt|7.08|m}} tall<ref>{{cite web |title=Airbus A300-600ST Beluga |publisher = Aerospace Technology |language = en-gb |url=https://www.aerospace-technology.com/projects/stbeluga/}}</ref>
<!--
        Powerplant
-->
|eng1 number=2
|eng1 name=[[General Electric CF6-80C2A8]]
|eng1 type=[[turbofan]]
|eng1 kn=257
|eng1 note=
<!--
        Performance
-->
|max speed kmh=
|max speed note=
|max speed mach=0.7 Maximum Operating Mach – MMO<ref name=TCDS/>
|cruise speed kmh=
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed note=
|range km=2779
|range note=with {{cvt|40|t|lb}} payload – {{cvt|4632|km|nmi}} with {{cvt|26|t|lb}} payload
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=10668
|ceiling note=<ref name=TCDS/>
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate note=
|time to altitude=
|wing loading kg/m2=
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}