Difference between revisions of "Mk-55 "Thud" Liquid Fuel Engine/Box"

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<noinclude>{{Data template used}}</noinclude>
 
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{{Infobox/Part
 
{{Infobox/Part
|file=Mark 55 Radial mount engine.png
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|file=Mk-55 Radial mount engine.png
 
|type=lfe
 
|type=lfe
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|size=r
 
|manufacturer=RMC
 
|manufacturer=RMC
 
|costs=820
 
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|filename=liquidEngineMk55.cfg
 
|filename=liquidEngineMk55.cfg
 
|part=liquidEngineMk55
 
|part=liquidEngineMk55
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|parent=Engine
 
|more={{Infobox/Part/reaction engine
 
|more={{Infobox/Part/reaction engine
|thrust=108.1967213
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|thrust=120
|isp-atm=275
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|isp-atm=275
|isp-vac=305
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|isp-vac=305
|vectoring=8
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|vectoring=8
|fuel=lfox
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|fuel=lfox
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=127
|staging=True
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|event=y
|event=True
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|staging=y
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}}
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{{Infobox/Part/cargo
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|volume=-1
 
}}
 
}}
 
}}
 
}}

Latest revision as of 20:22, 9 October 2024

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
Mk-55 "Thud" Liquid Fuel Engine
Part image
Liquid fuel engine by
Rockomax Conglomerate

Radial size Radial mounted
Cost (total) 820.00 Funds
Mass (total) 0.900 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Advanced rocketry.png Advanced Rocketry
Unlock cost 3 500 Funds
Since version 0.16
Part configuration liquidEngineMk55.cfg
Maximum thrust (1 atm) 108.20 kN
(vacuum) 120.00 kN
Isp (1 atm) 275 s
(vacuum) 305 s
Fuel consumption 8.02 Units of fuel/s
Thrust vectoring 8 °
Testing Environments
On the surface Yes
In the ocean Yes
On the launchpad Yes
In the atmosphere Yes
Sub-orbital Yes
In an orbit Yes
On an escape Yes
Docked No
Test by staging Yes
Manually testable Yes
Packed volume None