The l = 2 spherical harmonic expansion coefficients of the sky brightness distribution between 0.5 and 7 MHz

Open Access

Fig. 1

Antenna system of PSP. The four sensors V1, V2, V3, and V4 are mounted to and coplanar with the spacecraft heat shield, which is located in the back of the diagram. Radiator fins extend from the heat shield to a 1.5 m long hexagonal spacecraft bus in the foreground. The and directions shown define the spacecraft coordinate system.

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