The Eu:CROPIS Mass Property Campaign: Trimming a Spin-Stabilized Compact Satellite for a Long-Term Artificial Gravity Experiment

Table 9

Deployed configuration analysis results.

	Deployed flight
	Min	Mean	Max
(kgm^2)	42.978	43.317	43.565
(kgm^2)	43.371	43.548	43.773
(kgm^2)	48.670	48.916	49.207
Angle deviation (°)	-2.02	2.19	5.66
/ (-)	1.133	1.129	1.13
/ (-)	1.009	1.005	1.005