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Template:Rocketspecs/sandbox

From Wikipedia, the free encyclopedia

Testing location

Put the template code here and experiment with it.

Put your test example at Template:Rocketspecs/testcases

And there use {{Rocketspecs/sandbox |param= |param= |etc }}

General characteristics

  • Type:
  • Length:
  • Diameter:
  • Dry weight:

Components

  • Pumps:

Performance

This template provides formatted output for aircraft rocket engine specifications per Wikipedia:WikiProject Aircraft/page content. To use this template, copy-paste the following text:

{{rocketspecs
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
<!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> -->
|ref=
|type=
|length=
|diameter=
|weight=
|fueltype=
|oxidiser=
|capacity=
|pumps=
|thrust=
|thrust/weight=
|burn time=
|fuelcon=
|specfuelcon=
}}

See Template talk:Jettemp for explanation of parameters.