Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"
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|file=J33WheesleyBasicJetEngine.png | |file=J33WheesleyBasicJetEngine.png | ||
|type=je | |type=je | ||
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|manufacturer=C7 | |manufacturer=C7 | ||
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|filename=jetEngineBasic.cfg | |filename=jetEngineBasic.cfg | ||
| − | |part= | + | |part=jetEngines |
| − | |more= | + | |parent=Engine |
| − | {{Infobox/Part/jet engine | + | |more={{Infobox/Part/jet engine |
| − | | | + | |thrust=120 |
| − | |isp=10500 | + | |isp=10500 |
| − | | | + | |intake=127 |
| − | | | + | }} |
| + | {{Infobox/Part/generator | ||
| + | |generate=4 | ||
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
| − | |environments=15 | + | |environments=15 |
| − | |event= | + | |event=y |
| − | |staging= | + | |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 | |
