Delta II: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
Tidak ada ringkasan suntingan Tag: Suntingan perangkat seluler Suntingan peramban seluler |
Tidak ada ringkasan suntingan Tag: Suntingan perangkat seluler Suntingan peramban seluler |
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Baris 112:
|propmass = <!--propellant mass carried by a single stage in kilograms, use {{cvt}}, optional-->
|engines = 1 [[RS-27]] (6000 series) or [[RS-27A]] (7000 series) <ref>{{cite web|url=http://www.boeing.com/defense-space/space/delta/delta2/delta2.htm|title=Archived copy|access-date=November 3, 2006 |url-status=dead|archive-url=https://web.archive.org/web/20061103194958/http://www.boeing.com/defense-space/space/delta/delta2/delta2.htm|archive-date=November 3, 2006}}</ref>
|thrust =
|SI =
|burntime = 265
|fuel = [[RP-1]] / [[LOX]]
}}
Baris 127:
|propmass = <!--propellant mass carried by a single stage in kilograms, use {{cvt}}, optional-->
|engines = 1 [[AJ-10|AJ10-118K]]
|thrust =
|SI =
|burntime = 431
|fuel = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[Aerozine 50]]
}}
Baris 143:
|engines = [[Star 48B]]
|solid = yes
|thrust =
|SI =
|burntime = 87
|propellant = Aluminum fuel, ammonium perchlorate oxidizer in an HTPB binder
}}
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