Method for Predicting the Liquid-Sloshing Characteristics of a Microsatellite Propulsion System

Table 20

Simulation results of liquid storage tank and microsatellite with the deployment mechanism.

No.	(s)	(°/s)	(°/s)	(°/s)	(%)	(°/s)	(°/s)	(°/s)	Computation time in ABAQUS (s)
1	5	16	4	16	90	2.649	0.716	1.883	6993
2	6	2	12	14	10	0.375	1.839	1.547	2696
3	10	10	14	12	100	1.536	2.273	1.278	15,109
4	3	12	6	4	20	1.793	0.98	0.391	1725
5	4	4	20	6	80	0.541	3.145	0.593	5664
6	1	18	16	10	40	2.906	2.589	1.001	1708
7	2	8	8	20	60	1.143	1.265	2.289	3565
8	8	14	18	18	30	2.203	2.917	2.119	4708
9	9	6	2	8	50	0.835	0.366	0.802	7356
10	7	20	10	2	70	3.191	1.563	0.298	7333