RS-25: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
k from en:Space Shuttle main engine 16 October 2015, at 21:21. |
k Robot: Perubahan kosmetika |
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|fuel=[[Liquid hydrogen]]
|oxidiser=[[Liquid oxygen]]
|thrust(SL)={{convert|418000|lbf|kN|abbr=on|sigfig=3}}<ref name=
|thrust(Vac)={{convert|512300|lbf|kN|abbr=on|sigfig=4|lk=on}}<ref name=
|specific_impulse_vacuum={{convert|452.3|isp}}<ref name=
|specific_impulse_sea_level={{convert|366|isp}}<ref name=
|chamber_pressure={{convert|2994|psi|MPa|abbr=on}}<ref name=
|cycle=[[Staged combustion cycle (rocket)|Staged combustion]]
|nozzle_ratio=69:1 <ref name=
|length={{convert|168|in|m}}
|diameter={{convert|96|in|m}}
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{{Rocket Engines}}
== External Links ==
{{Commons category|Space Shuttle main engines}}
{{Include-NASA}}
* [http://nasatech.net/ntSSMEPF_PAGE.html Spherical panoramas of RS-25D in SSME Processing Facility prior to shipping to Stennis Space Center]
[[Kategori:Mesin roket]]
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