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. 27, 2020

Filed:

Jan. 05, 2018
Applicant:

Planet Labs Inc., San Francisco, CA (US);

Inventors:

Jedd Perry, San Francisco, CA (US);

Narinder Kumar, San Francisco, CA (US);

Kelly Hering, San Francisco, CA (US);

Kevin Meissner, San Francisco, CA (US);

Bayard Gardineer, San Francisco, CA (US);

Benjamin Howard, San Francisco, CA (US);

Assignee:

Planet Labs, Inc., San Francisco, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/22 (2006.01); B64G 1/64 (2006.01); B32B 1/00 (2006.01); H01C 7/10 (2006.01); H01C 7/13 (2006.01);
U.S. Cl.
CPC ...
B64G 1/222 (2013.01); B32B 1/00 (2013.01); B64G 1/641 (2013.01); B64G 1/645 (2013.01); H01C 7/10 (2013.01); H01C 7/13 (2013.01); B64G 2001/643 (2013.01);
Abstract

In one embodiment, an apparatus is attached to a feature to be deployed on a satellite. The apparatus includes a first material having an impedance, a second material coupled to the first material configured to provide a current or voltage to the first material causing the first material to generate heat based on the impedance after a launch process of a launch vehicle carrying the satellite has completed, and a third material configured to change state at a transition temperature. A release mechanism is coupled to the third material and holds the feature in an undeployed position on the satellite. The heat generated by the second material causes the third material to change state when the transition temperature range is reached and the release mechanism is released from the third material when the third material is in the second state to deploy the feature.


Find Patent Forward Citations

Perry, Jedd. (2020). Restraint system for deployment of a feature on a satellite (U.S. Patent No. 10815011). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10815011

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

Loading…