Difference between revisions of "J-404 "Panther" Afterburning Turbofan/Box"

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Latest revision as of 11:25, 18 August 2018

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
J-404 "Panther" Afterburning Turbofan
Part image
Jet engine by
C7 Aerospace Division

Radial size Small
Cost (total) 2 000.00 Funds
Mass (total) 1.200 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Supersonic flight.png Supersonic Flight
Unlock cost 9 000 Funds
Since version 1.0.5
Part configuration jetEngineAfterburning.cfg
Jet engine
Maximum thrust 85.00 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 130.00 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