Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"
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− | {{Infobox/Part | + | <noinclude>{{Data template used}}</noinclude>{{Infobox/Part |
− | |file= | + | |file=J33WheesleyBasicJetEngine.png |
− | |size= | + | |type=je |
− | |costs= | + | |size=1 |
− | |mass=1 | + | |manufacturer=C7 |
+ | |costs=1400 | ||
+ | |mass=1.5 | ||
|drag=0.2 | |drag=0.2 | ||
− | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
− | | | + | |research=Aerodynamics |
− | | | + | |unlock cost=4000 |
− | |||
− | |||
− | |||
− | |||
− | |||
|since=0.15 | |since=0.15 | ||
− | |part= | + | |filename=jetEngineBasic.cfg |
− | | | + | |part=jetEngines |
+ | |parent=Engine | ||
+ | |more={{Infobox/Part/jet engine | ||
+ | |thrust=120 | ||
+ | |isp=10500 | ||
+ | |intake=127 | ||
+ | }} | ||
+ | {{Infobox/Part/generator | ||
+ | |generate=4 | ||
+ | }} | ||
+ | {{Infobox/Part/test subject | ||
+ | |environments=15 | ||
+ | |event=y | ||
+ | |staging=y | ||
+ | }} | ||
+ | {{Infobox/Part/cargo | ||
+ | |volume=-1 | ||
+ | |stack=1 | ||
+ | }} | ||
}} | }} |
Latest revision as of 20:14, 9 October 2024
J-33 "Wheesley" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Radial size | Small | |
Cost | (total) | 1 400.00 |
Mass | (total) | 1.500 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 7 m/s | |
Research | Aerodynamics | |
Unlock cost | 4 000 | |
Since version | 0.15 | |
Part configuration | jetEngineBasic.cfg | |
Maximum thrust | 120.00 kN | |
Isp | (max) | 10500 s |
Fuel consumption | 0.23 /s | |
Intake air consumption | 29.60 /s | |
Thrust vectoring | No | |
Electricity generated | 4 ⚡/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 |