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

Table 7

Stowed flight configuration analysis results.

	Stowed flight
(kgm^2)	32.835
(kgm^2)	33.134
M3 (kgm^2)	34.702
Angle deviation (°)	4.6
/ (-)	1.057
/ (-)	1.009