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

Table 13

Simulation results of empty storage tank and microsatellite.

No.	(s)	(°/s)	(°/s)	(°/s)	(°/s)	(°/s)	(°/s)	Computation time in ABAQUS (s)
1	5	16	4	16	7.97	1.963	8.108	238
2	6	2	12	14	0.799	6.163	7.462	248
3	10	10	14	12	5.478	7.036	6.264	347
4	3	12	6	4	6.063	3.176	2.11	181
5	4	4	20	6	1.934	10.699	3.305	196
6	1	18	16	10	8.976	8.481	5.196	131
7	2	8	8	20	3.801	4.206	10.137	156
8	8	14	18	18	7.7	9.287	9.232	303
9	9	6	2	8	2.951	1.002	4.069	317
10	7	20	10	2	10.436	4.868	1.068	259