Falcon 9 Full Thrust: Perbedaan antara revisi

Konten dihapus Konten ditambahkan
Tidak ada ringkasan suntingan
Tidak ada ringkasan suntingan
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|name = Falcon 9 Full Thrust
|image = [[Berkas:ORBCOMM-2 (23802549782).jpg|280px]]
|caption = Launch ofPeluncuran the firstpertama Falcon 9 v1.2 (Full Thrust) flight,yang [[Falconmembawa 9muatan Flightsatelit 20]], carrying 11 [[Orbcomm (satellite)|Orbcomm]] satellites to orbit. [[Falcon 9 first-stage landing tests|The first stage was recovered]] atdi [[Cape Canaveral Air Force Station]] [[Landing Zones 1 and 2|LZ-1]] following the first successful Falcon 9 landing.
|function = [[Orbital spaceflight|Orbital]] [[medium-lift launch vehicle]]
|manufacturer = [[SpaceX]]
|country-origin = United[[Amerika StatesSerikat]]
|cpl = $62M (2016),<ref name=spacex-capabilities>{{cite web|title=Capabilities & Services (2016)|url=http://www.spacex.com/about/capabilities|publisher=SpaceX|accessdate=3 May 2016|date=2012-11-28}}</ref> $50M (2018)<ref>{{cite news |url=https://www.nasaspaceflight.com/2018/05/block-5-spacex-increase-launch-cadence-lower-prices/ |title=With Block 5, SpaceX to increase launch cadence and lower prices |first=Michael |last=Baylor |work=[[NASASpaceFlight.com]] |date=17 May 2018 |access-date=24 May 2018}}</ref>
|height = {{cvt|71|m|ft}} with payload fairing<ref name="spx-user-guide">{{cite web|title=Falcon 9 Launch Vehicle Payload User's Guide|url=http://www.spacex.com/sites/spacex/files/falcon_9_users_guide_rev_2.0.pdf|access-date=29 November 2015|date=21 October 2015|archive-url=https://web.archive.org/web/20170314002928/http://www.spacex.com/sites/spacex/files/falcon_9_users_guide_rev_2.0.pdf|archive-date=14 March 2017|url-status=dead}}</ref>
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|capacities = <!--insert one of the following templates for each payload:-->
{{Infobox rocket/payload
|location = [[LowOrbit Earthbumi orbitrendah|LEOOBR]] (28.5°)
|kilos = {{plainlist|
* Expendable: {{cvt|22,800|kg}},<ref name=spacex-capabilities /> {{cvt|15600|kg}} when landing
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}}
{{Infobox rocket/payload
|location = [[GeosynchronousOrbit transfer orbitgeostasioner|GTOOGS]] (27°)
|kilos = {{plainlist|
* Expendable: {{cvt|8,300|kg}}<ref name=spacex-capabilities/>
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}}
{{Infobox rocket/payload
|location = [[MarsOrbit transfer orbitMars|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/>
}}