SPACECRAFT PROPULSION SYSTEM WITH GYROSCOPIC MECHANISM |
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| 申请号 | PCT/TR2008000116 | 申请日 | 2008-09-24 | 公开(公告)号 | WO2009041928A2 | 公开(公告)日 | 2009-04-02 |
| 申请人 | TERZIAKIN MEHMET; | 发明人 | TERZIAKIN MEHMET; | ||||
| 摘要 | A propulsion method employing gyroscopes with electric motors which are being moved along a closed path in the spacecraft. Rotation axis of the gyroscopes are rotated periodically relative to movement direction so that gyroscopic effect is only obtained during movement in one direction. Thereby a gyroscopic resistance difference is obtained and used as a propulsion force. Another application is to use gyroscopes connected to generators in order to decelerate a spacecraft, transforming the moment created in gyroscope during deceleration into the electrical energy, distribute it to the space as heat transfer by means of radiation through the heat resistant panels. | ||||||
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| 说明书全文 | |||||||
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