J-404 "Panther" Afterburning Turbofan/Box

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J-404 "Panther" Afterburning Turbofan
Part image
Jet engine by
C7 Aerospace Division
Radial size Small
Cost (total) 2 000.00 Fund
Mass (total) 1.20 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Supersonic flight.png Supersonic Flight
Unlock cost 9000 Fund
Since version 1.0.5
Part configuration jetEngines
Jet engine
Maximum thrust 85 kN
Isp (max) 9000 s
Fuel con­sumption 0.19 units of fuel/s
Intake air consumption 7.70 Air unit/s
Thrust vectoring 10 °
Maximum thrust 130 kN
Isp (max) 4000 s
Fuel con­sumption 0.66 units of fuel/s
Intake air consumption 7.95 Air unit/s
Thrust vectoring 10 °
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