Difference between revisions of "J-404 "Panther" Afterburning Turbofan/Box"
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|type=je | |type=je | ||
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|manufacturer=C7 | |manufacturer=C7 | ||
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|unlock cost=9000 | |unlock cost=9000 | ||
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|part=jetEngines | |part=jetEngines | ||
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− | |more={{Infobox/Part/ | + | |more={{Infobox/Part/jet engine |
+ | |thrust=85 | ||
+ | |isp=9000 | ||
+ | |vectoring=10 | ||
+ | |intake=40 | ||
+ | }} | ||
{{Infobox/Part/jet engine | {{Infobox/Part/jet engine | ||
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− | |isp= | + | |isp=4000 |
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{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
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− | |event= | + | |event=y |
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Latest revision as of 20:15, 9 October 2024
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 | |
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 ° | |
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 |