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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
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
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 0.04 units of fuel/s
Intake air consumption 0.63 Air unit/s
Thrust vectoring 3 °