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:
Dec. 30, 1986

Filed:

Dec. 24, 1984
Applicant:
Inventor:

Mark S Yuan, Fountain Valley, CA (US);

Assignee:

Hughes Aircraft Company, Los Angeles, CA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G / ;
U.S. Cl.
CPC ...
2441 / ;
Abstract

An ejection mechanism for imparting an ejection force to substantially constant locus of points on a payload ejected from a spacecraft is disclosed. The ejection mechanism includes a rod having a contact end for abutting contact with the locus of points. The rod is slideably mounted within a housing defining a first aperture from which the rod is driven toward the locus of points. Means are provided for driving the rod toward the payload to eject the payload, and means are provided for securing the housing to the spacecraft. The ejection mechanism also includes means for permitting the contact end of the rod to substantially maintain abutting contact with the locus of points as the rod is driven toward the locus and the payload is ejected from the spacecraft.


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Yuan, Mark. (1986). Spacecraft payload ejection mechanism (U.S. Patent No. 4632339). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/4632339

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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