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Figure 1.
Different arrangements of the main satellite subsystems: (A) remote sensing satellite [15] and (B) Ionospheric Observation Nanosatellite Formation [16].
Figure 2.
Burn wire release mechanism in contact with white holding string [17].
Figure 3.
Antenna deployment mechanism: (A) deployed and (B) folded [18].
Figure 4.
Different geometries and sizes of small satellites: (A) CubeSat standardisation [20] and (B) one-unit hexagonal satellite [21] and (C) two-unit hexagonal satellite [22].
Figure 5.
Geometric parameters of the isogrid structure, where t is the rib height, x is the rib width and z is the rib thickness [28].
Figure 6.
Honeycomb sandwich panel structure [36].
Figure 7.
Geometric parameters of the honeycomb sandwich structure [37].