The invention provides a
spacecraft overall structure suitable for expansion of a T-shaped
assembly of a space
station. The
spacecraft overall structure comprises a working cabin, a multi-purpose cabin, a node cabin and a non-bearing propulsion cabin. On the basis of the configuration scheme,
layout area planning of large outboard equipment is provided, and installation of functional equipment such as a large-area semi-rigid plate
solar cell wing, a
thermal control fluid loop, a radiator and a propelling device can be supported. The configuration enables the
spacecraft to fully use the uplink envelope space of a carrier
rocket, supports in-cabin carrying of large-scale equipment, and has autonomous flight and active rendezvous and docking capabilities; in the
assembly stage, the T-shaped space
station assembly forms a cross-shaped structure through the structure, sufficient sealed cabins, energy, heat dissipation and other resources are provided for the whole
station, and
butt joint and parking support is provided for visiting aircrafts and subsequent cabin sections. A large opening is formed in the radial direction of the multipurpose cabin to the ground, large equipment in the cabin is supported to be deployed out of the cabin, double inner pressure-bearing cabin
doors are adopted, and the sealing safety of the space in the cabin is improved; by arranging the large observation window on the inner layer bearing cabin door, the space station has the safe direct ground observation capability.