The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 24, 2017

Filed:

May. 07, 2013
Applicant:

Beijing Institute of Spacecraft Environment Engineering, Beijing, CN;

Inventors:

Zhong Yi, Beijing, CN;

Chao Zhang, Beijing, CN;

Lifei Meng, Beijing, CN;

Haifu Jiang, Beijing, CN;

Yenan Liu, Beijing, CN;

Qi Xiao, Beijing, CN;

Lixiang Jiang, Beijing, CN;

Zhaoji Yu, Beijing, CN;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); F03H 1/00 (2006.01);
U.S. Cl.
CPC ...
B64G 1/405 (2013.01); B64G 1/409 (2013.01); F03H 1/0012 (2013.01); F03H 1/0037 (2013.01); F03H 1/0081 (2013.01); F03H 1/0093 (2013.01);
Abstract

A fuel-free spacecraft propelling system having an open-ended outer cylinder of a propelling device and an atomic oxygen collecting device is disclosed. The latter is arranged at the forwardly-propelled front end of the outer cylinder and is hermetically connected with an RF generating device and an ion cyclotron wave heating device through a magnetic confinement device. A spiral wave discharge oxygen plasma inlet and a spiral wave discharge oxygen plasma outlet in the ion cyclotron wave heating device are respectively provided with another magnetic confinement device. The propulsion of the invention does not need to carry the propellant, which greatly reduces the launch costs, and enables a spacecraft to advantageously have an increased orbit life over existing spacecraft systems.


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