A spacecraft that operates in a circular 425-km low-Earth orbit has a battery with 4 kW load at 28 VDC. Considering an average cell voltage of 1.5 V, and a maximum discharge depth of 50 %, what is the required weight of the battery made by: (a) Ni-Cd battery kg

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Space Vehicle Design20202020202020202020
A spacecraft that operates in a circular 425-km low-Earth orbit
has a battery with 4 kW load at 28 VDC. Considering an average
cell voltage of 1.5 V, and a maximum discharge depth of 50 %,
what is the required weight of the battery made by:
(a) Ni-Cd battery
kg
(b) Li-lon battery
kg
(c) Li-lon battery with 80% maximum discharge depth
kg
Specifications:
Ni-Cd: 39 Wh/kg
Li-lon: 80 Wh/kg
Transcribed Image Text:Space Vehicle Design20202020202020202020 A spacecraft that operates in a circular 425-km low-Earth orbit has a battery with 4 kW load at 28 VDC. Considering an average cell voltage of 1.5 V, and a maximum discharge depth of 50 %, what is the required weight of the battery made by: (a) Ni-Cd battery kg (b) Li-lon battery kg (c) Li-lon battery with 80% maximum discharge depth kg Specifications: Ni-Cd: 39 Wh/kg Li-lon: 80 Wh/kg
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