Difference between revisions of "Kerbodyne KR-2L+ "Rhino" Liquid Fuel Engine/Box"

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Revision as of 10:08, 30 April 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).
Kerbodyne KR-2L+ "Rhino" Liquid Fuel Engine
Part image
Liquid fuel engine by
Kerbodyne

Radial size Extra large
Cost (total) 21 000.00 Funds
Mass (total) 8.500 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Tech tree very heavy rocketry.png Very Heavy Rocketry
Unlock cost 64 000 Funds
Since version 0.23.5
Part configuration part.cfg
Maximum thrust (1 atm) 500.00 kN
(vacuum) 1 000.00 kN
Isp (1 atm) 170 s
(vacuum) 340 s
Fuel consumption 59.98 Units of fuel/s
Thrust vectoring 4 °
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