J-33 "Wheesley" Turbofan Engine/Box
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< J-33 "Wheesley" Turbofan Engine
Revision as of 18:48, 17 March 2017 by Sal vager (talk | contribs) (Reverted edits by Rocketing Rudolph (talk) to last revision by UmbralRaptor)
| 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 |  Aerodynamics
| |
| Unlock cost | 4 000
| |
| Since version | 0.15 | |
| Part configuration | jetEngineBasic.cfg | |
| Maximum thrust | 120.00 kN | |
| Isp | (max) | 9600 s |
| Fuel consumption | 0.25  /s
| |
| Intake air consumption | 0.00  /s
| |
| Thrust vectoring | No | |
| 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 | |
