Falcon Heavy: Тафовут байни таҳрирҳо
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{{Infobox rocket
|
| image= Falcon_Heavy_cropped.jpg|| caption= Falcon Heavy on pad [[Kennedy Space Center Launch Complex 39|LC-39A]], being prepared for its first launch.
| function= [[Orbital spaceflight|Orbital]] [[super heavy-lift launch vehicle]]
| manufacturer =[[SpaceX]]
| country-origin= United States
| cpl= $90M for up to 26,700 kg to GTO<ref name="Capabilities & Services">{{cite web|url=http://www.spacex.com/about/capabilities |title=Capabilities & Services |author= |date= |publisher=SpaceX |accessdate=August 21, 2017}}</ref>
| height= {{cvt|70|m}}<ref name="sxfh">{{cite web |title=Falcon Heavy |url=http://www.spacex.com/falcon-heavy |publisher=SpaceX |accessdate=April 5, 2017}}</ref>
| diameter= {{cvt|3.66|m}}<ref name="sxfh"/>
| width= {{cvt|12.2|m}}<ref name="sxfh"/>
| mass= {{cvt|1,420,788|kg}}<ref name="sxfh"/>
| stages= 2+
<!----Payloads (optional)---->
|capacities= <!--insert one of the following templates for each payload:-->
{{Infobox rocket/payload
|location= [[Low Earth orbit|LEO]] (28.5°) <!--Target orbit/trajectory, required. Please use [[Geostationary transfer orbit|GTO]] or [[Low Earth orbit|LEO]] instead of just [[GTO]] or [[LEO]].-->
|kilos = {{cvt|63,800|kg}}<ref name="sxfh"/> <!--Payload mass in kilograms, use {{convert|PAYLOAD|kg|abbr=on}}, required-->
}}
{{Infobox rocket/payload
|location= [[Geosynchronous transfer orbit|GTO]] (27°) <!--Target orbit/trajectory, required. Please use [[Geostationary transfer orbit|GTO]] or [[Low Earth orbit|LEO]] instead of just [[GTO]] or [[LEO]].-->
|kilos = {{cvt|26,700|kg}}<ref name="sxfh"/> <!--Payload mass in kilograms, use {{convert|PAYLOAD|kg|abbr=on}}, required-->
}}
{{Infobox rocket/payload
|location= [[Mars transfer orbit|Mars]] <!--Target orbit/trajectory, required. Please use [[Geostationary transfer orbit|GTO]] or [[Low Earth orbit|LEO]] instead of just [[GTO]] or [[LEO]].-->
|kilos = {{cvt|16,800|kg}}<ref name="sxfh"/> <!--Payload mass in kilograms, use {{convert|PAYLOAD|kg|abbr=on}}, required-->
}}
{{Infobox rocket/payload
|location= [[Hohmann transfer orbit#Application to interplanetary travel|Pluto]] <!--Target orbit/trajectory, required. Please use [[Geostationary transfer orbit|GTO]] or [[Low Earth orbit|LEO]] instead of just [[GTO]] or [[LEO]].-->
|kilos = {{cvt|3500|kg}}<ref name="sxfh"/> <!--Payload mass in kilograms, use {{convert|PAYLOAD|kg|abbr=on}}, required-->
}}
<!----Associated rockets (optional)---->
|family = [[Falcon 9]] <!--rocket family, optional-->
|derivatives = <!--derived rockets, optional-->
|comparable = {{flatlist|
* [[Delta IV Heavy]]
* [[Long March 5]]
* [[New Glenn]]
* [[Saturn C-3]]
* [[Vulcan (rocket)|Vulcan]]
}}<!--similar, unrelated rockets, optional-->
<!----Launch history (required)---->
| status= Active
| sites= {{plainlist|
* [[Kennedy Space Center|Kennedy]] [[LC-39A]]
* [[SpaceX South Texas Launch Site]] (under construction)
}}
| launches= 1
| success= 1 <!-- Note these are labeled LAUNCH Successes, not mission successes. -->
| fail= 0 <!-- LAUNCH failures only to match label in Infobox. -->
| partial= 0
| first= February 6, 2018<ref name=elon_tweet_27jan>{{cite tweet |user=elonmusk |author=Elon Musk|number=957361443023695872 |date=January 27, 2018 |title=Aiming for first flight of Falcon Heavy on Feb 6 from Apollo launchpad 39A at Cape Kennedy. Easy viewing from the public causeway.}}</ref><ref name=SFinsider_sch>{{cite web |author= |url= http://www.spaceflightinsider.com/launch-schedule/ |title= Launch Calendar |date= |accessdate= January 25, 2018}}</ref>
<!--Stages/boosters-->
|stagedata =
{{Infobox rocket/stage
|type = booster <!--booster or stage (must be in lower case)-->
|diff = <!--variant of rocket this is used on, optional-->
|stageno = <!--position of stage in rocket, spelled out (eg. First, Second, etc), required-->
|name = <!--name of the stage/booster, optional-->
|number = 2 <!--number of boosters, required if type= booster-->
|length = <!--length of a single booster/stage in metres, use {{convert|LENGTH|m|abbr=on}}, optional-->
|diameter = <!--diameter of a single booster/stage in metres, use {{convert|DIAMETER|m|abbr=on}}, optional-->
|width = <!--width of a single booster/stage if not axisymmetric, use {{convert|WIDTH|m|abbr=on}}, optional-->
|empty = <!--empty mass of a single booster/stage in kilograms, use {{convert|EMPTYMASS|kg|abbr=on}}, optional-->
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{convert|GROSSMASS|kg|abbr=on}}, optional-->
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{convert|PROPMASS|kg|abbr=on}}, optional-->
|engines = 9 [[Merlin 1D]] <!-- [[Merlin (rocket engine)|Merlin 1Dnumber]] and type of engines used on each individual booster/stage, required-->
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = '''Sea level:''' {{cvt|7.6|MN}} (each) <br /> '''Vacuum:''' {{cvt|8.2|MN}} (each)
|total = '''Sea level:''' {{cvt|15.2|MN}} <br /> '''Vacuum:''' {{cvt|16.4|MN}}
|SI = '''Sea level:''' 282 seconds<ref>{{cite web|title=Falcon 9|url=http://www.spacex.com/falcon9|publisher=SpaceX|accessdate=September 29, 2013|archiveurl=https://web.archive.org/web/20130501002858/http://www.spacex.com/falcon9|archivedate=May 1, 2013}}</ref> <br />'''Vacuum''': 311 seconds<ref name=msF9Study>{{cite web|author1=Ahmad, Taseer|author2=Ammar, Ahmed|author3=Kamara, Ahmed|author4=Lim, Gabriel|author5=Magowan, Caitlin|author6=Todorova, Blaga|author7=Tse, Yee Cheung|author8=White, Tom|title=The Mars Society Inspiration Mars International Student Design Competition|url=http://members.marssociety.org/inspiration-mars/honorablementions/Spectre%20Mars_UnivOfGlasgow.pdf|website=Mars Society|accessdate=October 24, 2015}}</ref> <!--specific impulse of an individual booster/stage, in secs, optional-->
|burntime = 154 seconds
|fuel = [[Subcooling|Subcooled]] [[LOX]] / Chilled [[RP-1]]<ref name="musk-tweet-20151217">{{cite tweet |user=elonmusk |number=677666779494248449 |author-link=Elon Musk |date=December 17, 2015 |title= -340 F in this case. Deep cryo increases density and amplifies rocket performance. First time anyone has gone this low for O2. [RP-1 chilled] from 70F to 20 F |accessdate= December 19, 2015}}</ref> <!--fuel used in stage/boosters, required-->
}}
{{Infobox rocket/stage
|type = stage <!--booster or stage (must be in lower case)-->
|diff = <!--variant of rocket this is used on, optional-->
|stageno = First <!--position of stage in rocket, spelled out (eg. First, Second, etc), required-->
|name = <!--name of the stage/booster, optional-->
|number = <!--number of boosters, required if type= booster-->
|length = <!--length of a single booster/stage in metres, use {{convert|LENGTH|m|abbr=on}}, optional-->
|diameter = <!--diameter of a single booster/stage in metres, use {{convert|DIAMETER|m|abbr=on}}, optional-->
|width = <!--width of a single booster/stage if not axisymmetric, use {{convert|WIDTH|m|abbr=on}}, optional-->
|empty = <!--empty mass of a single booster/stage in kilograms, use {{convert|EMPTYMASS|kg|abbr=on}}, optional-->
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{convert|GROSSMASS|kg|abbr=on}}, optional-->
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{convert|PROPMASS|kg|abbr=on}}, optional-->
|engines = 9 [[Merlin 1D]] <!-- number and type of engines used on each individual booster/stage, required-->
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = '''Sea level:''' {{cvt|7.6|MN}} <br /> '''Vacuum:''' {{cvt|8.2|MN}}
|SI = '''Sea level:''' 282 seconds <br />'''Vacuum:''' 311 seconds <!--specific impulse of an individual booster/stage, in secs, optional-->
|burntime = 187 seconds <!--burn time, required-->
|fuel = [[Subcooled]] [[LOX]] / Chilled [[RP-1]] <!--fuel used in stage/boosters, required-->
}}
{{Infobox rocket/stage
|type = stage <!--booster or stage (must be in lower case)-->
|diff = <!--variant of rocket this is used on, optional-->
|stageno = Second <!--position of stage in rocket, spelled out (eg. First, Second, etc), required-->
|name = <!--name of the stage/booster, optional-->
|number = <!--number of boosters, required if type= booster-->
|length = <!--length of a single booster/stage in metres, use {{convert|LENGTH|m|abbr=on}}, optional-->
|diameter = <!--diameter of a single booster/stage in metres, use {{convert|DIAMETER|m|abbr=on}}, optional-->
|width = <!--width of a single booster/stage if not axisymmetric, use {{convert|WIDTH|m|abbr=on}}, optional-->
|empty = <!--empty mass of a single booster/stage in kilograms, use {{convert|EMPTYMASS|kg|abbr=on}}, optional-->
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{convert|GROSSMASS|kg|abbr=on}}, optional-->
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{convert|PROPMASS|kg|abbr=on}}, optional-->
|engines = 1 [[Merlin 1D Vacuum]] <!-- [[Merlin (rocket engine)|Merlin 1Dnumber]] and type of engines used on each individual booster/stage, required-->
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = {{cvt|934|kN}}<ref name="sxfh"/> <!--thrust provided by a single booster/stage in kN, use {{convert|THRUST|kN|abbr=on}}, required-->
|SI = 348 seconds<ref name="sxfh"/>
|burntime = 397 seconds<ref name="sxfh"/> <!--burn time, required-->
|fuel = [[LOX]] / [[RP-1]] <!--fuel used in stage/boosters, required-->
}}
}}
'''Falcon Heavy''' (букв. {{tr-en|Сокол (тяжёлый)}}) — [[США|американская]] [[ракета-носитель]] сверхтяжёлого класса семейства [[Falcon (ракеты)|Falcon]], созданная компанией [[SpaceX]].
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