Abstract: It discloses a dexamethasone-loaded macrophage-derived microvesicle as well as a preparation method and application thereof. The dexamethasone-loaded macrophage-derived microvesicle is formed by entrapping dexamethasone with a microvesicle derived from a murine macrophage cell line 264.7 cell. The dexamethasone-loaded macrophage-derived microvesicle of the present invention can be taken up by an injured cell more effectively, and fulfills the aim of ameliorating the kidney inflammation by inhibiting the activation of a proinflammatory signal pathway and infiltration of inflammatory cells. Meanwhile, the preparation method of the present invention is simple, convenient and efficient, and the prepared microvesicle is derived from the RAW 264.7 cells which are sufficient and widespread, and can be produced in large-scale.

Abstract: A spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery includes: S1, enabling a delivery connection rod to be slidably connected to two mass blocks in a length direction, and adjusting the center of mass of a spacecraft system to pass through a main connecting shaft; S2, respectively measuring, calibrating and adjusting the center of mass and the principal axis of inertia of the delivery connection rod that is to deliver the space target or de-orbit debris; S3, carrying out energy storage delivery; S4, respectively adjusting the center of mass and the moment of inertia of the delivery connection rod after delivering the space target or de-orbit debris; S5, carrying out energy dissipation and unloading; and S6, enabling the spacecraft system to prepare to grab the next space target or de-orbit debris and proceeding to the next delivery work cycle.

Abstract: A spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery includes: S1, enabling a delivery connection rod to be slidably connected to two mass blocks in a length direction, and adjusting the center of mass of a spacecraft system to pass through a main connecting shaft; S2, respectively measuring, calibrating and adjusting the center of mass and the principal axis of inertia of the delivery connection rod that is to deliver the space target or de-orbit debris; S3, carrying out energy storage delivery; S4, respectively adjusting the center of mass and the moment of inertia of the delivery connection rod after delivering the space target or de-orbit debris; S5, carrying out energy dissipation and unloading; and S6, enabling the spacecraft system to prepare to grab the next space target or de-orbit debris and proceeding to the next delivery work cycle.