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 | ||
+ | |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= | + | |more={{Infobox/Part/title|je}} |
{{Infobox/Part/jet engine | {{Infobox/Part/jet engine | ||
+ | |intake=227 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) --> | ||
|isp=12600 | |isp=12600 | ||
|thrust=360 | |thrust=360 | ||
Line 25: | Line 26: | ||
|area=0.03 | |area=0.03 | ||
|max=3.4 | |max=3.4 | ||
+ | }} | ||
+ | {{Infobox/Part/test subject | ||
+ | |environments=15 | ||
+ | |event=True | ||
+ | |staging=True | ||
}} | }} | ||
}} | }} |
Latest revision as of 09:43, 11 April 2019
J-90 "Goliath" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Radial size | Radial mounted | |
Cost | (total) | 2 600.00 |
Mass | (total) | 4.50 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Volume | ? | |
Impact Tolerance | 7 m/s | |
Research | Heavy Aerodynamics | |
Unlock cost | 15 000 | |
Since version | 1.0.5 | |
Part configuration | jetEngineBig.cfg | |
Jet engine | ||
Maximum thrust | 360 kN | |
Isp | (max) | 12600 s |
Fuel consumption | 0.58 /s | |
Intake air consumption | 132.27 /s | |
Thrust vectoring | No | |
Intake speed | 30 | |
Intake area | 0.03 m2 | |
Maximum intake air | 3.4 | |
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 |