Overall design of remote sensing large-platform satellite for on orbit assembly and maintenance

Abstract

Aiming at the envelope constraint problem of carrier rocket fairing, based on the design idea of on orbit assembly and maintenance, in this paper a general design scheme of a remote sensing large-platform satellite (RSLPS) that can realize large scale multi-load collaborative observation is proposed. The basic process of on orbit assembly is introduced, and the composition, structural form and technical principle of the universal interface design, micro vibration control design and thermal deformation control design of the load platform are expounded. The proposed design scheme provides a valuable choice for the research of RSLPS based on on orbit assembly and maintenance.