J-404 "Panther" Afterburning Turbofan

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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 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
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 °
Electricity generated 5.0 ⚡/s
Electricity generated 3.0 ⚡/s
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
Packed volume None
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A thrust vectoring jet engine with two modes. The first mode, Dry mode, is similar to that of the wheesley, with a bit more thrust. The second mode, Wet mode, uses the afterburner to produce thrust almost equal to the Whiplash Turboramjet. This can make it a good alternative for when you want something that can be controllable and doesn't need excessive heat shielding, but still need to be able to go incredibly fast if necessary, at the expense of increase fuel consumption.

Product description

A high performance jet engine with a variable geometry thrust vectoring nozzle and an afterburner for extra thrust.

Changes

1.0.5
  • Initial release