Editing Payload (section)

==Examples==
Examples of payload capacity:
*[[de Havilland Mosquito]] B Mk.IV Series 2: 920&nbsp;kg<ref>Jackson, Robert. de Havilland Mosquito (Combat Legend), page 15. Shrewsbury, UK: Airlife Publishing Ltd., 2003. ISBN 1-84037-358-X.</ref>
*[[Boeing B-17 Flying Fortress]]: 1,800&nbsp;kg (typical long range missions), 3,600&nbsp;kg or more (short range missions)<ref>{{Cite web |date=2024-03-06 |title=B-17 {{!}} Crew, Range, & Bomb Load {{!}} Britannica |url=https://www.britannica.com/technology/B-17 |access-date=2024-04-04 |website=www.britannica.com |language=en}}</ref>
*[[Petlyakov Pe-8]] 4,990&nbsp;kg (internal)<ref>{{Cite web |title=Petlyakov Pe-8 (TB-7) Long-Range Strategic Heavy Bomber Aircraft Specifications and Pictures |url=https://www.militaryfactory.com/aircraft/detail.php?aircraft_id=1146 |access-date=2024-04-04 |website=www.militaryfactory.com}}</ref>
*[[B-52H Stratofortress]]: 31,500&nbsp;kg<ref>{{Cite web |title=B-52H Stratofortress |url=https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104465/b-52h-stratofortress/https://www.af.mil/About-Us/Fact-Sheets/Display/Article/104465/b-52h-stratofortress/ |access-date=2024-04-04 |website=Air Force |language=en-US}}{{dead link|date=March 2025|bot=medic}}{{cbignore|bot=medic}}</ref>
*[[Antonov An-225 Mriya|Antonov An-225 ''Mriya'']]: 250,000&nbsp;kg
*[[Saturn V]]:
**Payload to [[Low Earth Orbit]] 140,000&nbsp;kg
**Payload to Lunar orbit 47,000&nbsp;kg
*[[Space Shuttle]]:
**Payload to Low Earth Orbit (Not counting the 110,000&nbsp;kg serviced orbiter) 27,000&nbsp;kg (53,700&nbsp;lb)
**Payload to [[geostationary transfer orbit]] (Not counting the 110,000&nbsp;kg serviced orbiter) 3,810&nbsp;kg (8,390&nbsp;lb)
*[[Trident (missile)]]: 2800&nbsp;kg [[throw weight]] {{specify|date=February 2015}}{{citation needed|date=February 2015}}
*[[Automated Transfer Vehicle]]
**Payload:<ref>{{Cite web |title=Utilisation Relevant Data |url=https://esamultimedia.esa.int/docs/ATV/FS003_12_ATV_updated_launch_2008.pdf |access-date=2024-04-04}}</ref> 7,667&nbsp;kg 8 racks with 2 x 0.314 m<sup>3</sup> and 2 x 0.414 m<sup>3</sup>
**Envelope: each 1.146 m<sup>3</sup> in front of 4 of these 8 racks
**Cargo mass: Dry cargo: 1,500 - 5,500&nbsp;kg
**Water: 0 – 840&nbsp;kg
**Gas (Nitrogen, Oxygen, air, 2 gases/flight): 0 – 100&nbsp;kg
**ISS Refueling propellant: 0 – 860&nbsp;kg (306&nbsp;kg of fuel, 554&nbsp;kg of oxidizer)
**ISS re-boost and attitude control propellant: 0 - 4,700&nbsp;kg
**Total cargo upload capacity: 7,667&nbsp;kg