Delta IV: Perbedaan antara revisi

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Tidak ada ringkasan suntingan
Tag: Suntingan perangkat seluler Suntingan peramban seluler
Tidak ada ringkasan suntingan
Tag: Suntingan perangkat seluler Suntingan peramban seluler
Baris 38:
* [[Proton-M]]
}}
|status = [[Delta IV Heavy]] isadalah activesistem peluncuran aktif; Delta IV Medium, M+(4,2), M+(5,2), and M+(5,4) retiredsudah pensiun.
|sites = [[Cape Canaveral Space Launch Complex 37|SLC-37B]], [[Cape Canaveral Air Force Station|Cape Canaveral]]<br/>[[Vandenberg Space Launch Complex 6|SLC-6]], [[Vandenberg Air Force Base|Vandenberg AFB]]
 
Baris 62:
|first = {{plainlist|
* '''Medium/M+:''' 20 November 2002 ([[Eutelsat W5]])
* '''Heavy:''' 21 DecemberDesember 2004 ([[List of USA satellites|USA-181]])
}}
|last= {{plainlist|
* '''Medium/M+:''' 22 AugustAgustus 2019 ([[USA-293]]/[[GPS satellite blocks|GPS III-2]])
* '''Heavy:''' 10 DecemberDesemember 2020 ([[List of NRO launches|NROL-44]])
}}
|payloads = {{flatlist|
* [[Geostationary Operational Environmental Satellite|GOES]]
 
* [[GPS Block IIF]]
 
* [[NROL|NRO classified payloads]]
 
* [[Wideband Global SATCOM|WGS]]
 
* [[Exploration Flight Test 1]]
 
* [[Parker Solar Probe]]
}}
Baris 90 ⟶ 95:
|thrust = {{cvt|826.6|kN}}
|total = <!-- total thrust for all boosters in kN, use {{cvt}}, optional -->
|SI = {{cvt|245|isp}} (seapermukaan levellaut)
|burntime = 91 secondsdetik
|fuel = [[Hydroxyl-terminated polybutadiene|HTPB]] / [[Aluminum]]
}}
{{Infobox rocket/stage
Baris 105 ⟶ 110:
|propmass = <!-- propellant mass carried by a single booster in kilograms, use {{cvt}}, optional -->
|engines = 1 [[RS-68A]]
|thrust = {{cvt|705000|lbf|kN|order=flip}} (seapermukaan levellaut)
|total = <!-- total thrust for all boosters in kN, use {{cvt}}, optional -->
|SI = '''[[SeaPermukaan levellaut]]:''' {{cvt|360|isp}}<br/>'''[[VacuumHampa udara]]:''' {{cvt|412|isp}}
|burntime = 242 secondsdetik<ref name=":1"/>
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}
{{Infobox rocket/stage
|type = stageTingkat
|diff =
|stageno = FirstPertama
|name = [[Common Booster Core]] (CBC)
|number = 2
Baris 123 ⟶ 128:
|propmass = <!-- propellant mass carried by a single stage in kilograms, use {{cvt}}, optional -->
|engines = 1 [[RS-68A]]
|thrust = {{cvt|705,000|lbf|kN|order=flip}} (seapermukaan levellaut)
|SI = '''[[SeaPermukaan levellaut]]:''' {{cvt|360|isp}}<br/>'''[[VacuumHampa udara]]:''' {{cvt|412|isp}}
|burntime = 245 secondsdetik (328 secondsdetik indalam Heavykonfigurasi configurationHeavy)<ref name=":1"/>
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}
{{Infobox rocket/stage
|type = stageTingkat
|diff =
|stageno = SecondKedua
|name = [[Delta Cryogenic Second Stage]] (DCSS)
|number = 1
Baris 142 ⟶ 147:
|thrust = {{cvt|110|kN|lbf}}
|SI = {{cvt|462|isp}}
|burntime = 850-1,125 secondsdetik
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}