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.
Patent No.:
Date of Patent:
Oct. 21, 1986
Filed:
Apr. 15, 1983
Applicant:
Inventor:
John E Keigler, Princeton, NJ (US);
Assignee:
RCA Corporation, Princeton, NJ (US);
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G / ; B64G / ;
U.S. Cl.
CPC ...
2441 / ; 244165 ;
Abstract
An improved system and method of ejecting a spacecraft from a shuttle or orbiter type craft in space includes a momentum wheel on the spacecraft that has a spin axis parallel to the ejection direction, spinning-up this momentum wheel prior to ejection and after ejection de-spinning this wheel whereby the whole spacecraft spins without the need of a spin table on the shuttle or orbiter craft.
Quick Actions:
Keigler, John. (1986). Spacecraft angular momentum stabilization system and method (U.S. Patent No. 4618112). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/4618112
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile