{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()