Difference between revisions of "J-33 "Wheesley" Turbofan Engine/Box"
From Kerbal Space Program Wiki
m (*update to 1.0;) |
m (*update to 1.0.2;) |
||
| Line 16: | Line 16: | ||
|more= | |more= | ||
{{Infobox/Part/jet engine | {{Infobox/Part/jet engine | ||
| + | |isp=19200 | ||
|thrust=115 | |thrust=115 | ||
|vectoring=1 | |vectoring=1 | ||
| − | |||
}} | }} | ||
{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
|environments=71 | |environments=71 | ||
| + | |event=True | ||
|staging=True | |staging=True | ||
| − | |||
}} | }} | ||
}} | }} | ||
Revision as of 18:59, 3 May 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 | 115.00 kN | |
| Isp | (max) | 19200 s |
| Fuel consumption | 0.12  /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 | |
