CR-7 R.A.P.I.E.R. Engine/Box

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CR-7 R.A.P.I.E.R. Engine
Part image
Hybrid engine by
C7 Aerospace Division and Rockomax Conglomerate
Radial size Small
Cost (total) 6 000.00 Fund
Mass (total) 2.00 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 20 m/s
Research Aerospace tech.png Aerospace Tech
Unlock cost 35000 Fund
Since version 0.23
Part configuration rapierEngine
Liquid fuel engine
Maximum thrust (1 atm) 162.30 kN
(vacuum) 180.00 kN
Isp (1 atm) 275 s
(vacuum) 305 s
Fuel con­sumption 12.02 units of fuel/s


Thrust vectoring 3 °
Jet engine
Maximum thrust 105 kN
Isp (max) 3200 s
Fuel con­sumption 0.67 units of fuel/s
Intake air consumption 4.01 Air unit/s
Thrust vectoring 3 °
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