Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"
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{{Infobox/Part | {{Infobox/Part | ||
|file=J-90 Goliath Turbofan Engine.png | |file=J-90 Goliath Turbofan Engine.png | ||
| − | |||
|type=je | |type=je | ||
| − | | | + | |size=r |
| + | |manufacturer=C7 | ||
|costs=2600 | |costs=2600 | ||
|mass=4.5 | |mass=4.5 | ||
| + | |ia=3.4 | ||
| + | |drag=0.2 | ||
| + | |temp=2000 | ||
|tolerance=7 | |tolerance=7 | ||
| − | |||
| − | |||
|research=Heavy Aerodynamics | |research=Heavy Aerodynamics | ||
|unlock cost=15000 | |unlock cost=15000 | ||
| − | | | + | |since=1.0.5 |
|filename=jetEngineBig.cfg | |filename=jetEngineBig.cfg | ||
|part=jetEngines | |part=jetEngines | ||
| − | |more= | + | |parent=Engine |
| + | |more={{Infobox/Part/air intake | ||
| + | |speed=30 | ||
| + | |area=0.03 | ||
| + | }} | ||
{{Infobox/Part/jet engine | {{Infobox/Part/jet engine | ||
| − | |isp=12600 | + | |thrust=360 |
| − | | | + | |isp=12600 |
| − | | | + | |intake=227 |
| + | }} | ||
| + | {{Infobox/Part/generator | ||
| + | |generate=16 | ||
| + | }} | ||
| + | {{Infobox/Part/test subject | ||
| + | |environments=15 | ||
| + | |event=y | ||
| + | |staging=y | ||
}} | }} | ||
| − | {{Infobox/Part/ | + | {{Infobox/Part/tank |
| − | | | + | |ia=3.4 |
| − | |||
| − | |||
}} | }} | ||
}} | }} | ||
Latest revision as of 20:16, 9 October 2024
| J-90 "Goliath" Turbofan Engine | ||
 | ||
| Jet engine by C7 Aerospace Division | ||
| Radial size | Radial mounted | |
| Cost | (total) | 2 600.00 
|
| (dry) | 2 600.00
| |
| Mass | (total) | 4.517 t |
| (dry) | 4.517 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 | |
| Intake speed | 30 m/s | |
| Intake area | 3 m2 | |
| Maximum thrust | 360.00 kN | |
| Isp | (max) | 12600 s |
| Fuel consumption | 0.58  /s
| |
| Intake air consumption | 132.27  /s
| |
| Thrust vectoring | No | |
| Electricity generated | 16 ⚡/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 | |
| Intake air | 3
| |
