Falcon 9 Full Thrust: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
Nadiantara (bicara | kontrib) Tidak ada ringkasan suntingan |
Nadiantara (bicara | kontrib) Tidak ada ringkasan suntingan |
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Baris 70:
|type = stage <!--booster or stage (must be in lower case)-->
|diff = <!--variant of rocket this is used on, optional-->
|stageno =
|name = <!--name of the stage/booster, optional-->
|number = <!--number of boosters, required if type = booster-->
Baris 82:
|solid = <!--set to "yes" (lowercase) to change Engines to Motor for solid motors-->
|thrust = '''Sea level:''' {{cvt|7,607|kN|}}<ref name=spacex-falcon9/> <br />'''Vacuum:''' {{cvt|8,227|kN|}}<ref name=spacex-falcon9 />
|SI = '''Sea level:''' 282 detik<ref name=falcon9-2013>{{cite web|title=Falcon 9 |url=http://www.spacex.com/falcon9.php |publisher=SpaceX |accessdate=29 September 2013 |archiveurl=https://web.archive.org/web/20130501002858/http://www.spacex.com/falcon9.php |archivedate=1 May 2013|date=2012-11-16 }}</ref>{{Update after|2013|9|reason=ISP for first-stage Merlin 1D is taken from v1.1 specs, new source required}} <br/> '''Vacuum''': 311
|burntime = 162 detik<ref name=spacex-falcon9 /> <!--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=2015-12-17 |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 = 19 December 2015}}</ref> <!--fuel used in stage/boosters, required-->
Baris 89:
|type = stage <!--booster or stage (must be in lower case)-->
|diff = <!--variant of rocket this is used on, optional-->
|stageno =
|name = <!--name of the stage/booster, optional-->
|number = <!--number of boosters, required if type = booster-->
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