Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"
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Peteletroll (talk | contribs) |
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|mass=4.5 | |mass=4.5 | ||
|tolerance=7 | |tolerance=7 | ||
| − | |temp=2000 | + | |temp=2000 |
|drag=0.2 | |drag=0.2 | ||
|research=Heavy Aerodynamics | |research=Heavy Aerodynamics | ||
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|isp=12600 | |isp=12600 | ||
|thrust=360 | |thrust=360 | ||
| − | |vectoring= | + | |vectoring= |
}} | }} | ||
{{Infobox/Part/air intake | {{Infobox/Part/air intake | ||
Revision as of 05:22, 26 November 2015
| J-90 "Goliath" Turbofan Engine | ||
 | ||
| Jet engine by C7 Aerospace Division | ||
| Cost | (total) | 2 600.00 
|
| Mass | (total) | 4.500 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Heavy Aerodynamics
| |
| Unlock cost | 15 000
| |
| Since version | 1.0.5 | |
| Part configuration | jetEngineBig.cfg | |
| Maximum thrust | 360.00 kN | |
| Isp | (max) | 12600 s |
| Fuel consumption | 0.58  /s
| |
| Intake air consumption | 0.00  /s
| |
| Thrust vectoring | No | |
| Intake speed | 30 m/s | |
| Intake area | 3 m2 | |
