Difference between revisions of "User:XZise/Part"
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(Underline. I couldnt get it to center) |
m (*use the second manufacturer option;) |
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{{Infobox/Part | {{Infobox/Part | ||
|file=Rapier_Engine_01.png | |file=Rapier_Engine_01.png | ||
| − | |manufacturer=C7 Aerospace Division | + | |manufacturer=C7 Aerospace Division |
| + | |manufacturer2=Rockmax Conglomerate | ||
|size=s | |size=s | ||
|costs=5900 | |costs=5900 | ||
| Line 9: | Line 10: | ||
|tolerance=20 | |tolerance=20 | ||
|since=0.23 | |since=0.23 | ||
| − | |part= | + | |part=rapierEngine |
| + | |parent=Engine | ||
|role=Hybrid engine | |role=Hybrid engine | ||
|more= | |more= | ||
| − | {{Infobox/Line| | + | {{Infobox/Line|'''Liquid fuel engine'''|style=text-align:center;text-decoration:underline;}} |
{{User:XZise/Part/LFE | {{User:XZise/Part/LFE | ||
|thrust=175 | |thrust=175 | ||
| Line 19: | Line 21: | ||
|vectoring=3 | |vectoring=3 | ||
}} | }} | ||
| − | {{Infobox/Line|'''Jet engine'''}} | + | {{Infobox/Line|'''Jet engine'''|style=text-align:center;text-decoration:underline;}} |
{{User:XZise/Part/JE | {{User:XZise/Part/JE | ||
|thrust=190 | |thrust=190 | ||
| − | | | + | |stall=? |
| + | |isp=800 | ||
|vectoring=3 | |vectoring=3 | ||
}} | }} | ||
| Line 34: | Line 37: | ||
* Also some parameters are superfluous (e.g. vectoring) | * Also some parameters are superfluous (e.g. vectoring) | ||
:: This might be only the case here, but maybe future other hybrid engines have different vectoring values? | :: This might be only the case here, but maybe future other hybrid engines have different vectoring values? | ||
| + | |||
| + | → [[Template_talk:Infobox/Part#Rework_the_template.3F|Discussion]] | ||
Latest revision as of 18:02, 28 December 2013
| XZise | ||
 | ||
| Hybrid engine by C7 Aerospace Divisionand Rockmax Conglomerate | ||
| Radial size | Small | |
| Cost | (total) | 5 900.00 
|
| Mass | (total) | 1.750 t |
| Drag | 0.2 | |
| Max. Temp. | 3600 K | |
| Impact Tolerance | 20 m/s | |
| Research | Unknown | |
| Unlock cost | 0
| |
| Since version | 0.23 | |
| Part configuration | [[Parts/Engine/rapierEngine/{{{filename}}}|{{{filename}}}]] | |
| Liquid fuel engine | ||
| Maximum thrust | (1 atm) | 155.56 kN |
| (vacuum) | 175.00 kN | |
| Isp | (1 atm) | 320 s |
| (vacuum) | 360 s | |
| Thrust vectoring | 3 ° | |
| Jet engine | ||
| Maximum thrust | 190 kN | |
| Stall Threshold | ? kN | |
| Isp | 800 s
Template:Infobox/Part/FuelConsumption Template:Infobox/Part/FuelConsumption | |
| Thrust vectoring | 3 ° | |
This is an example how I "envision" the next generation of part templates. Current problems with this system:
- Most of the names are already used
- There might be a workaround: Use the same name for both templates, but if the mass parameter is determined it treats it as the old version?
- There might be multiple properties with the same name (e.g. maximum thrust)
- I added headers here manually, in the final version, those headers should be integrated in the subtemplates. Maybe rearrange them, that research and since are not below the specific ones (or separate them with another header)
- Also some parameters are superfluous (e.g. vectoring)
- This might be only the case here, but maybe future other hybrid engines have different vectoring values?
