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 Divisionand Rockomax Conglomerate

Radial size Small
Cost (total) 6 000.00 Funds
Mass (total) 2.000 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 20 m/s
Research Aerospace tech.png Aerospace Tech
Unlock cost 35 000 Funds
Since version 0.23
Part configuration rapierEngine.cfg
Maximum thrust 105.00 kN
Isp (max) 3200 s
Fuel consumption 0.67 Units of fuel/s
Intake air consumption 4.02 Air unit/s
Thrust vectoring 3 °
Maximum thrust (1 atm) 162.30 kN
(vacuum) 180.00 kN
Isp (1 atm) 275 s
(vacuum) 305 s
Fuel consumption 12.04 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 Yes
In an orbit Yes
On an escape Yes
Docked No
Test by staging Yes
Manually testable Yes