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:
Mar. 20, 2018

Filed:

Sep. 01, 2016
Applicant:

The United States of America As Represented BY the Administrator of the National Aeronautics and Space Administration, Washington, DC (US);

Inventors:

Joseph M. Davila, West Friendship, MD (US);

Douglas M. Rabin, Arnold, MD (US);

Nelson Reginald, Bryans Road, MD (US);

Qian Gong, Columbia, MD (US);

Neerav Shah, Columbia, MD (US);

Phillip C. Chamberlin, Gambrills, MD (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01J 1/04 (2006.01); G01J 1/44 (2006.01); B64G 1/24 (2006.01); B64G 1/10 (2006.01); G01J 1/02 (2006.01); G01J 1/42 (2006.01); G01S 3/786 (2006.01); B64G 1/26 (2006.01); B64G 1/40 (2006.01);
U.S. Cl.
CPC ...
G01J 1/0437 (2013.01); B64G 1/105 (2013.01); B64G 1/26 (2013.01); B64G 1/406 (2013.01); G01J 1/0266 (2013.01); G01J 1/0271 (2013.01); G01J 1/4228 (2013.01); G01J 1/44 (2013.01); G01S 3/7861 (2013.01); G01J 2001/4266 (2013.01); G01J 2001/446 (2013.01);
Abstract

The present invention relates to a space-based instrument which provides continuous coronal electron temperature and velocity images, for a predetermined period of time, thereby improving the understanding of coronal evolution and how the solar wind and Coronal Mass Ejection transients evolve from the low solar atmosphere through the heliosphere for an entire solar rotation. Specifically, the present invention relates to using a 6U spherical occulter coronagraph CubeSat, and a relative navigational system (RNS) that controls the position of the spacecraft relative to the occulting sphere. The present invention innovatively deploys a free-flying spherical occulter, and after deployment, the actively controlled CubeSat will provide an inertial formation flying with the spherical occulter and Sun.


Find Patent Forward Citations

Loading…