Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"
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|intake=127 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) --> | |intake=127 <!-- Amount of Air required per 1 unit of LF (Calc: Air / LF) --> |
Revision as of 11:25, 18 August 2018
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 | |
Jet engine | ||
Maximum thrust | 120.00 kN | |
Isp | (max) | 10500 s |
Fuel consumption | 0.23 /s | |
Intake air consumption | 29.60 /s | |
Thrust vectoring | No | |
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 |