Title:
SPIRAL-PROPULSION-TYPE SPACECRAFT LAUNCHING METHOD
Document Type and Number:
WIPO Patent Application WO/2023/116520
Kind Code:
A1
Abstract:
Disclosed herein is a spiral-propulsion-type spacecraft launching method, which comprises a method for launching a spacecraft from a celestial body in the solar system and a method for launching a spacecraft toward the outside of the solar system. Key operations comprise: first, reducing the initial velocity of a spacecraft that is obtained as same self-rotates or revolves with a celestial body; and then adjusting, to be in the same straight line, the thrust and flight direction of the spacecraft and the gravitational force of an escaped celestial body to which the spacecraft is subjected, and such method is the most ideal method. The present invention is applicable to a spacecraft which has a large mass, which is at a high orbit, or which performs more distant exploration; and is helpful in improving the utilization efficiency of the thrust of a spacecraft.
More Like This:
| JPH0542898 | MULTIPLE STAGE ROCKET |
| WO/2021/081389 | LAUNCH AND FLIGHT CONFIGURATIONS FOR TRANSFER SPACE VEHICLES |
| WO/2023/212682 | LOW GRAVITY POWER DISTRIBUTION SYSTEM AND DEVICE |
Inventors:
CHEN XIAOBIN (CN)
Application Number:
PCT/CN2022/138889
Publication Date:
June 29, 2023
Filing Date:
December 14, 2022
Export Citation:
Assignee:
CHEN XIAOBIN (CN)
International Classes:
B64G1/00; B64G1/40
Foreign References:
| CN114229035A | 2022-03-25 | |||
| CN104139872A | 2014-11-12 | |||
| CN101220785A | 2008-07-16 | |||
| CN113775496A | 2021-12-10 | |||
| CN104309822A | 2015-01-28 | |||
| US20180278322A1 | 2018-09-27 |
Attorney, Agent or Firm:
SU ZHOU ZHONG HE INTELLECTUAL PROPERTY FIRM (CN)
Download PDF:
Previous Patent: BATTERY SOC ESTIMATION METHOD AND RELATED APPARATUS
Next Patent: CONTROL METHOD AND APPARATUS FOR ELECTRONIC DEVICE, AND DEVICE
Next Patent: CONTROL METHOD AND APPARATUS FOR ELECTRONIC DEVICE, AND DEVICE