Difference between revisions of "J-404 "Panther" Afterburning Turbofan/Box"
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Revision as of 11:25, 18 August 2018
J-404 "Panther" Afterburning Turbofan | ||
Jet engine by C7 Aerospace Division | ||
Radial size | Small | |
Cost | (total) | 2 000.00 |
Mass | (total) | 1.200 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 7 m/s | |
Research | Supersonic Flight | |
Unlock cost | 9 000 | |
Since version | 1.0.5 | |
Part configuration | jetEngineAfterburning.cfg | |
Jet engine | ||
Maximum thrust | 85.00 kN | |
Isp | (max) | 9000 s |
Fuel consumption | 0.19 /s | |
Intake air consumption | 7.70 /s | |
Thrust vectoring | 10 ° | |
Maximum thrust | 130.00 kN | |
Isp | (max) | 4000 s |
Fuel consumption | 0.66 /s | |
Intake air consumption | 7.95 /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 |