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

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< CR-7 R.A.P.I.E.R. Engine
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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) 3 600.00 Funds
Mass (total) 1.20 t
Drag 0.2
Max. Temp. 3600 K
Volume  ?
Impact Tolerance 20 m/s
Research Hypersonic flight.png Hypersonic Flight
Unlock cost 35 000 Funds
Since version 0.23
Part configuration rapierEngine.cfg
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) 155.56 kN
(vacuum) 175.00 kN
Isp (1 atm) 320 s
(vacuum) 360 s
Fuel consumption 9.91 Units of fuel/s


Thrust vectoring 3 °
Jet engine
Maximum thrust 190 kN
Isp (max) 800 s
Fuel consumption 4.84 Units of fuel/s
Intake air consumption 0.00 Air unit/s
Thrust vectoring 3 °