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Auto Credit Based on davygravy10's IonX DrooSat V1.00 “Light Flare”

The second varient of the DrooSat and of the Light Flare spacecraft that will be used to research Juno.

GENERAL INFO

PERFORMANCE

  • Total Delta V: 0m/s
  • Total Thrust: 0N
  • Engines: 0
  • Wet Mass: 694kg
  • Dry Mass: 694kg

STAGES

Stage Engines Delta V Thrust Burn Mass

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