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:
Aug. 31, 1976

Filed:

Jun. 27, 1975
Applicant:
Inventors:

John Edward Keigler, Princeton, NJ (US);

Ludwig Muhlfelder, Livingston, NJ (US);

Robert Joseph Cenker, Princeton, NJ (US);

Assignee:

RCA Corporation, New York, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G / ;
U.S. Cl.
CPC ...
244169 ; 244322 ;
Abstract

A pair of reaction motors or thrusters connected to spin-stabilized spacecraft are used to reorient spacecraft attitude without affecting spacecraft velocity. The spacecraft reaction motors are arranged to produce a couple in response to an attitude reference signal without applying a spacecraft velocity changing force to the spin-stabilized spacecraft.


Find Patent Forward Citations

Keigler, John. (1976). Orientation system for a spin stabilized spacecraft (U.S. Patent No. 3977633). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/3977633

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

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