then
t
m/s
m/s2
to
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{{pack.name}}
{{type.name}}
{{part.name}}

Found {{bestStagingsValid}} Valid Rocket Designs (and {{bestStagingsCount}} Invalid)

Most Optimal Rocket Design Found!

Attempt #{{staging.attempt}}
Stage Part x Cost Mass (t) Delta-V (m/s) TWR Time (s)
{{$index}}
Asparagus
  1. {{part.name}} x{{part.count}}
  2. Payload: {{stage.payload}}t
  3. {{part.name}} x{{part.count}}
  4. {{part.name}} x{{part.count}}
  5. {{part.name}} x{{part.count}}
  6. {{part.name}} x{{part.count}}
  7. {{part.name}} x{{part.count}}
x{{stage.multiplier}} {{stage.costStage}} / {{stage.costTotal}} {{stage.massStage.toFixed(3)}} / {{stage.massTotal.toFixed(3)}} {{Math.round(stage.deltaVStage)}} / {{Math.round(stage.deltaVTotal)}} {{stage.twr.toFixed(2)}} {{stage.timeStage.toFixed(1)}} / {{stage.timeTotal.toFixed(1)}}