The invention relates to a rapid charge supply device for
spacecraft pulse charge emission, and belongs to the field of space charging and discharging. The bottom plate is of a plate-shaped structure which is horizontally arranged in the axial direction; the
cathode is of a cylindrical structure; the cathodes are in coaxial
butt joint; the
anode is of a cylinder structure; the
anode is coaxially arranged in the inner cavity of the
cathode; the root of the
anode is butted with the bottom plate; the working medium sleeves the outer wall of the middle part of the anode and is filled between the
cathode and the anode; the spring is sleeved on the outer wall of the anode root; one end of the spring is contacted with the bottom plate; one end of the spring contacts with the working medium end face; the insulating
assembly is arranged at the opening of the axial head end of the cathode; two poles of the energy compression module are respectively connected with the cathode and the anode; the power supply is connected with the energy compression module to charge the energy compression module; a charge self-consistent cavity is formed on the outer side of the opening of the axial head end of the cathode; when the device is used for
spacecraft pulse charge beam output, rapid supply in the pulse is achieved, and the
spacecraft is kept electrically neutral in real time.