ผลต่างระหว่างรุ่นของ "ฟัลคอน 9 บล็อค 5"
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{{Infobox rocket
|name = Falcon 9 Block 5
|image = File:Falcon 9 Demo-2 Launching 6 (3).jpg|Falcon 9 Demo-2 Launching 6 (3)
|image_size = <!--size of image (omit "px" suffix), optional, defaults to 270px-->
|caption = The Block 5 variant of the Falcon 9 launching Crew Dragon in Demo-2 mission from [[Kennedy Space Center]] on May 30, 2020. The rocket's distinguishing black thermal protection coating on the interstage is discernible.
|function = [[Reusable launch system|Partially reusable]] [[Orbital spaceflight|orbital]] [[medium-lift launch vehicle]]
|manufacturer = [[SpaceX]]
|country-origin = United States
|height = {{cvt|70|m}} with payload fairing<ref name="spx-user-guide-B5-update">{{cite web|title=Falcon User's Guide|url=https://www.spacex.com/media/falcon_users_guide_042020.pdf|accessdate=February 26, 2019|date=January 14, 2019}}</ref>
|diameter = {{cvt|3.66|m}}<ref name=spacex-falcon9>{{cite web|title=Falcon 9|url=https://www.spacex.com/vehicles/falcon-9/|publisher=SpaceX|accessdate=April 30, 2016|date=November 16, 2012}}</ref>
|mass = {{cvt|549054|kg}}<ref name=spacex-falcon9/>
|stages = 2
<!----Payloads (optional)---->
|capacities = <!--insert one of the following templates for each payload:-->
{{Infobox rocket/payload
|location = [[Low Earth orbit|LEO]] (28.5°)
|kilos = {{plainlist|
* Expendable: {{cvt|22800|kg}},<ref name=spacex-capabilities>{{cite web|title=Capabilities & Services (2016)|url=http://www.spacex.com/about/capabilities|publisher=SpaceX|accessdate=May 3, 2016|date=November 28, 2012}}</ref> {{cvt|15600|kg}} when landing
}}
}}
{{Infobox rocket/payload
|location = [[Geosynchronous transfer orbit|GTO]] (27°)
|kilos = {{plainlist|
* Expendable: {{cvt|8300|kg}}<ref name=spacex-capabilities/>
* Reusable: {{cvt|5500|kg}}<ref name=spacex-capabilities/>
}}
}}
{{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|4,020|kg}}<ref name=spacex-capabilities/>
}}
<!----Associated rockets (optional)---->
|family = [[Falcon 9]]
|derivatives = <!--derived rockets, optional-->
| comparable = {{flatlist|
* [[Atlas V#Variants|Atlas V 541]]
* [[H-IIB]]
* [[Long March 3B/E]]
* [[Proton-M]]
* [[Ariane 5#Variants|Ariane 5 ES]]
}}
<!----Launch history (required)---->
|status = Active
|launches = {{Falcon rocket statistics|F9FTBlock5launch}}
|success = {{Falcon rocket statistics|F9FTBlock5success}}
|fail = <!--total failed launches, optional-->
|partial = <!--total number of launches resulting in partial failure (e.g. incorrect orbit but still usable), optional-->
|other_outcome = <!--number of launches with unknown outcomes (or in progress), optional-->
|landings = <!--total number of landings, optional-->
|first = May 11, 2018
|payloads = {{plainlist|
* [[SpaceX Dragon]] / [[Crew Dragon]]
* [[GPS Block IIIA]]
* ''[[Beresheet]]'' lunar lander
}}
<!--Stages/boosters (optional)-->
|stagedata = <!--insert one of the following templates for each stage:-->
{{Infobox rocket/stage
|type = stage
|diff = <!--variant of rocket this is used on, optional-->
|stageno = First
|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 {{cvt|LENGTH|m}}, optional-->
|diameter = <!--diameter of a single booster/stage in metres, use {{cvt|DIAMETER|m}}, optional-->
|width = <!--width of a single booster/stage if not axisymmetric, use {{cvt|WIDTH|m}}, optional-->
|empty = <!--empty mass of a single booster/stage in kilograms, use {{cvt|EMPTYMASS|kg}}, optional-->
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{cvt|GROSSMASS|kg}}, optional-->
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{cvt|PROPMASS|kg}}, optional-->
|engines = 9 [[Merlin 1D]]+
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = {{cvt|7607|kN}}<ref>{{cite web|url=https://www.youtube.com/watch?v=rQEqKZ7CJlk|title=Bangabandhu Satellite-1 Mission|last=SpaceX|date=|publisher=|accessdate=February 2, 2019|via=YouTube}}</ref><ref>{{cite web|url=https://www.spacex.com/falcon9|title=FALCON 9|last=SpaceX|date=|publisher=SpaceX|accessdate=March 2, 2019 }}</ref>
|total = <!--total thrust for all boosters in kN, use {{cvt|THRUST|kN}}, optional-->
|SI = <!--specific impulse of an individual booster/stage, in seconds, use {{convert|ISP_IN_SECONDS|isp}}, optional-->
|burntime = <!--burn time, required-->
|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>
}}
{{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 {{cvt|LENGTH|m}}, optional-->
|diameter = <!--diameter of a single booster/stage in metres, use {{cvt|DIAMETER|m}}, optional-->
|width = <!--width of a single booster/stage if not axisymmetric, use {{cvt|WIDTH|m}}, optional-->
|empty = <!--empty mass of a single booster/stage in kilograms, use {{cvt|EMPTYMASS|kg}}, optional-->
|gross = <!--gross (fuelled) mass of a single booster/stage, use {{cvt|GROSSMASS|kg}}, optional-->
|propmass = <!--propellant mass carried by a single booster/stage in kilograms, use {{cvt|PROPMASS|kg}}, optional-->
|engines = 1 [[Merlin 1D Vacuum]]
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = {{cvt|934|kN}}<ref name=spacex-falcon9 />
|SI =
|burntime =
|fuel = LOX / RP-1
}}
}}
'''ฟัลคอน 9 บล็อค 5''' ({{lang-en|Falcon 9 Block 5}}) เป็น[[จรวดขนาดกลาง]][[แบบสองขั้นสู่วงโคจร]]ที่ออกแบบและผลิตในประเทศสหรัฐโดย [[SpaceX]] เป็นรุ่นที่ห้าของ [[Falcon 9 Full Thrust]] ซึ่งขับเคลื่อนโดยเครื่องยนต์ SpaceX [[Merlin]] ซึ่งเผาไหม้[[ออกซิเจนเหลว]] (LOX) และน้ำมันก๊าดเกรดจรวด ([[RP-1]])
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