Abstract: A solar power system for use with a space vehicle for achieving extended mission duration is disclosed. The solar power system includes sets of foldable solar panel casings which are unfolded and extended to the starboard and port sides (.+-.Y axis) of the space vehicle. During stowage the laterally offset sets of casings are placed in an overlapping arrangement to reduce the lateral space occupied within the payload bay of the host space vehicle. The casings are further extended away from the space vehicle by extending an extendable boom along the .+-.Y axis. The extendable boom preferably includes a first and second boom section rotatably attached at their inboard end of the support structure. The solar panels contained within the casings are extended in a .+-.Z axis and a hinge is provided between the ends of the boom sections ad the casings such that the deployed panels can rotate about the .+-.Z axis. A pitch drive motor rotates the boom sections about the .+-.Y axis.

Abstract: An acceleration free research laboratory is provided that is confined within a satellite but free of any physical engagement with the walls of the satellite, wherein the laboratory has adequate power, heating cooling and communications services to conduct basic research and development.An inner part containing the laboratory is positioned at the center-of-mass of a satellite within the satellite's outer shell. The satellite is then positioned such that its main axes are in a position parallel to its main axes are in a position parallel to its flight velocity vector or in the direction of the residual acceleration vector. When the satellite is in its desired orbit, the inner part is set free so as to follow that orbit without contacting the inside walls the outer shell.