Difference between revisions of "RV-1 "Cub" Vernier Engine/Box"

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Latest revision as of 21:02, 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).
RV-1 "Cub" Vernier Engine
Part image
Liquid fuel engine by
Reaction Systems Ltd

Radial size Tiny, Radial mounted
Cost (total) 800.00 Funds
Mass (total) 0.180 t
Drag 0.3-0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Precision propulsion.png Precision Propulsion
Unlock cost 3 200 Funds
Since version 1.4.1
Part configuration LiquidEngineRV-1.cfg
Maximum thrust (1 atm) 28.90 kN
(vacuum) 32.00 kN
Isp (1 atm) 280 s
(vacuum) 310 s
Fuel consumption 2.11 Units of fuel/s
Thrust vectoring 22.5 °
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 170 l