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

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|isp-atm=275
 
|isp-atm=275
 
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|vectoring=8
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{{Infobox/Part/test subject
 
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Revision as of 19:01, 3 May 2015

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
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 No
In an orbit No
On an escape No
Docked No
Test by staging Yes
Manually testable Yes