The invention provides an SAR
satellite structure suitable for multi-
satellite launching and a design method, and relates to the technical field of
spacecraft design, the SAR
satellite structure comprises a satellite main body, a solar wing, a
radiation unit, an
antenna substrate, a plate penetrating connector, a TR
assembly and a semi-rigid connection
assembly, the SAR satellite structure adopts a trapezoidal cross section configuration, the internal space of a
rocket fairing is fully utilized, and the space of the
rocket fairing is fully utilized; a heat conduction unit and a heating unit are arranged between the
radiation unit and the
antenna substrate and between the
antenna substrate and the TR
assembly, so that the
radiation array plane flatness of the radiation unit and the installation flatness of the TR assembly are ensured, heat conduction between single machines is increased, and the temperature consistency of the antenna is improved; the semi-rigid connection assembly can reduce the response of the active section antenna, release the
thermal deformation of the antenna, reduce the flatness change, improve the precision of a radiation array plane, and solve the problems that the space
utilization rate of an existing SAR satellite is low, the flatness of the antenna is easily affected by
thermal deformation, and the temperature of the antenna is difficult to control.