Difference between revisions of "48-7S "Spark" Liquid Fuel Engine/Box"

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Revision as of 14:23, 18 January 2017

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
48-7S "Spark" Liquid Fuel Engine
Part image
Liquid fuel engine by
Rockomax Conglomerate
Radial size Tiny
Cost (total) 240.00 Funds
Mass (total) 0.10 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Propulsion systems.png Propulsion Systems
Unlock cost 2 800 Funds
Since version 0.21
Part configuration liquidEngine48-7S
Maximum thrust (1 atm) 16.88 kN
(vacuum) 20.00 kN
Isp (1 atm) 270 s
(vacuum) 320 s
Fuel consumption 1.27 Units of fuel/s


Thrust vectoring 3 °
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