{0,8:0.0}       $&$ fc.PropellantStageCurrent()
{0,6:0.0}       $&$ fc.PropellantDelta()



{0,8:0.0}       $&$ fc.RcsStageCurrent()
{0,6:0.00}      $&$ fc.RcsDelta()




{0,8:0.0}       $&$ fc.PowerCurrent()
{0,6:0.00}      $&$ fc.PowerDelta()