De-orbiting Drag Sail

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Abstract:

This thesis examined the possibility of developing a compact, reliable, and scalable drag sail to aid in de-orbiting satellites during their end-of-life operations. Using a current prototype, we created and tested a full-scale drag sail. We also developed a reliable mechanism that both retains the drag sail in a stowed configuration to prevent mission obstruction and, when commanded, allows a smooth and successful deployment.

Author(s):
Nichols, Samuel J.
Author Organization(s):
Naval Postgraduate School
Funding Organization(s):
Publication Date:
2020 Jun 01
Pagination:
0

Security Markings

RECORD

Collection: TRECMS
Subject Terms
Modernization Areas:
Space
Communities of Interest:
No COI(s) Identified
Descriptor(s):
artificial satellites, space debris, low earth orbits, spacecraft, computer-aided design, space objects, space systems, environment, materials, outer space, release mechanisms, small satellites, space environments, governments, orbits, reliability, united states
Keyword(s):
drag sail, de orbit, scalable
Subject Categories:
Mechanical, Industrial, Civil and Marine Engineering
Update Date:
2020 Dec 07