No abstract

No abstract

No abstract

At launch the Cassini spacecraft holds 3100 kg of liquid propellant.With a dry mass of 2200 kg, the liquid propellant mass fraction is 60% at launch, indicating that an evaluation of the attitude control system would be incomplete without some capability t o model the dynamics of the propellant.In this paper, mechanlcalanalogy models for propellant slosh a r e developed using d a t a generated bv comp;tational fluid dynamics and statics currently for attitude control design and

No abstract