Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"
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Revision as of 22:24, 24 June 2015
J-33 "Wheesley" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Radial size | Small | |
Cost | (total) | 950.00 |
Mass | (total) | 1.500 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 7 m/s | |
Research | Aviation | |
Unlock cost | 4 000 | |
Since version | 0.15 | |
Part configuration | jetEngineBasic.cfg | |
Maximum thrust | 80.00 kN | |
Isp | (max) | 9600 s |
Fuel consumption | 0.17 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | 1 ° | |
Testing Environments | ||
On the surface | Yes | |
In the ocean | Yes | |
On the launchpad | Yes | |
In the atmosphere | No | |
Sub-orbital | No | |
In an orbit | No | |
On an escape | Yes | |
Docked | No | |
Test by staging | Yes | |
Manually testable | Yes |