Chinese Academy of Sciences

Shanghai Institutes of Biological Sciences, Cas

Haiyang Liu

Jinxing Zheng

Ming Li

Lin Nan Li

Lei Zhu

Quan Chen

Fei Liu

Xiaojiang Hao

Mingzhun Lei

Yifan Du

Ge Wang

Xiaoliang Zhu

Zhuoyao Tang

Cheng Zhou

Chen Yan

Zhou Yin

Xiaoli He

Pinghui Zhao

Yudong Lu

A high-temperature superconducting plasma thruster system, having variable temperature ranges and being applied in space, is provided. The high-temperature superconducting plasma thruster system includes: a cathode-anode assembly, a high-temperature superconducting magnet system, a supporting and adjusting platform, a power-and-gas supply and cooling system, and an obtaining control system. The cathode-anode assembly is disposed at a center of a ring of the high-temperature superconducting magnet system; the cathode-anode assembly and the high-temperature superconducting magnet system are spatially engaged with each other by the supporting and adjusting platform to form a main body of the thruster system; the power-and-gas supply and cooling system and the obtaining control system are located outside of the main body of the thruster system and are connected to the cathode-anode assembly and the high-temperature superconducting magnet system.

High-temperature superconducting plasma thruster system having variable temperature ranges and being applied in space

The present disclosure provides a cooling structure of heat pipe for superconducting magneto plasma dynamic thruster having a cylindrical structure and includes a cathode, an intermediate connector and an anode. The cathode is arranged inside the intermediate connector, the anode is arranged outside the intermediate connector; the cathode is provided with a cathode cooling mechanism, and the anode is provided with an anode cooling mechanism. The cathode cooling mechanism includes a cathode heat pipe and a cathode heat dissipation fin. The anode heat pipe cooling mechanism includes an anode heat pipe and an anode heat dissipation fin.

Cooling structure of heat pipe for superconducting magneto plasma dynamic thruster

The invention relates to a derivative of 15-oxospiramilacton, particularly to a compound of Formula I or II, or an isomer, a solvate or a pharmaceutically acceptable salt thereof. The invention also relates to a pharmaceutical composition comprising the compound as pharmaceutically active ingredient, a method for preparing the same, and use thereof in manufacture of an anti-tumor agent. The derivative of 15-oxospiramilactone of the invention have an activity against multiple tumor cell lines, and the anti-tumor activity is positively correlated to an activity inhibiting the Wnt signaling pathway. 

15-oxospiramilactone derivatives, preparation method and uses thereof

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Hefei, China

Haiyang Liu