Difference between revisions of "RE-J10 "Wolfhound" Liquid Fuel Engine/Box"

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Latest revision as of 21:01, 21 September 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).
RE-J10 "Wolfhound" Liquid Fuel Engine
Part image
Liquid fuel engine by
Rockomax Conglomerate

Radial size Large
Cost (total) 3 000.00 Funds
Mass (total) 3.300 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 6 m/s
Research Tech tree very heavy rocketry.png Very Heavy Rocketry
Unlock cost 12 000 Funds
Since version 1.4.1
Part configuration LiquidEngineRE-J10.cfg
Maximum thrust (1 atm) 69.08 kN
(vacuum) 375.00 kN
Isp (1 atm) 70 s
(vacuum) 380 s
Fuel consumption 20.13 Units of fuel/s
Thrust vectoring 3.0 °
Electricity generated 8.0 ⚡/s
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