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

Table 18

Simulation results of empty 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	2.596	0.677	1.826	1065
2	6	2	12	14	0.368	1.813	1.518	1247
3	10	10	14	12	1.489	2.212	1.231	1904
4	3	12	6	4	1.762	0.962	0.38	781
5	4	4	20	6	0.512	3.081	0.558	969
6	1	18	16	10	2.858	2.541	0.972	502
7	2	8	8	20	1.112	1.232	2.234	650
8	8	14	18	18	2.166	2.868	2.076	1548
9	9	6	2	8	0.809	0.345	0.774	1690
10	7	20	10	2	3.133	1.521	0.271	1429