Removing Orbital Debris with Less Risk-Reference-Cited by-同舟云学术

Removing Orbital Debris with Less Risk

Published:2013-03 Issue:2 Volume:50 Page:365-379
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Nock Kerry T.¹,Aaron Kim M.¹,McKnight Darren²

Affiliation:

1. Global Aerospace Corporation, Altadena, California 91001-5327

2. Integrity Applications Incorporated, Chantilly, Virginia 20151

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32286

Reference12 articles.

1. HoytR.ForwardR. “The Terminator Tether: Autonomous De-Orbit of LEO Spacecraft for Space Debris Mitigation,” AIAA Paper 2000-0329, 2000.

2. Refined algorithms for structural breakup due to hypervelocity impact

3. LiouJ.C.MatenyM. J.Anz-MeadorP. D.KesslerD.JansenM.TheallJ. R. “The New NASA Orbital Debris Engineering Model ORDEM2000,” NASA TP-2002-210780, May 2002.

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