On-Orbit Thermal Design and Validation of 1 U Standardized CubeSat of STEP Cube Lab

Table 10

On-orbit temperature prediction after thermal design modification on the battery.

Component	Without MLI on the battery (°C)			With MLI on the battery (°C)
	Hot operation	Cold operation	Cold emergency	Hot operation	Cold operation	Cold emergency
	panel	56.20	−43.90	−44.75	56.88	−44.12	−44.29
panel	49.89	−33.64	−34.52	52.15	−34.39	−34.41
panel	33.54	−42.08	−44.75	33.52	−41.90	−43.06
panel	−3.78	−39.13	−43.36	−2.37	−40.32	−40.58
I/F board	36.16	−25.60	−25.77	37.96	−25.51	−25.75
GPS board	15.67	−8.19	−8.80	18.24	−7.21	−9.91
OBC board	26.62	−15.68	−18.21	27.30	−15.53	−16.10
Comm. board	19.46	−9.47	−11.98	20.35	−9.55	−10.83
Power board	14.61	−20.49	−22.76	18.32	−20.47	−21.20
Battery	26.90	−3.78	−8.07	27.81	2.64	1.84
MEMS	30.96	−26.77	−30.41	29.46	−28.27	−28.57
SEC	58.20	−35.20	−36.18	59.45	−36.18	−36.04
PCM	19.52	−7.18	−9.39	20.36	−7.44	−8.64
HRM	17.25	2.03	−0.20	17.26	1.82	0.60