Difference between revisions of "User:XZise/Part"

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 Template:Infobox/Part/FuelConsumption
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?

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