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Disposal, Deployment, and Debris in Near Rectilinear Halo OrbitsA proposed Gateway facility in a lunar Near Rectilinear Halo Orbit (NRHO) will serve as an outpost in deep space, with spacecraft periodically arriving and departing. Departing objects will include logistics modules, requiring safe disposal, cubesats, deployed to various destinations, and debris objects, whose precise paths may be unknown. Escape dynamics from NRHOs are complex; primarily influenced by the Earth and Moon within the orbit, spacecraft are significantly impacted by solar gravity upon departure. The current investigation explores the dynamics of departure from the NRHO, including the risk of debris recontact, safe heliocentric disposal, and deployment to select destinations.
Document ID
20190000672
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Davis, Diane C.
(Jacobs Technology, Inc. Houston, TX, United States)
Boudad, Kenza K.
(Purdue Univ. West Lafayette, IN, United States)
Phillips, Sean M.
(a.i. solutions, Inc. Lanham, MD, United States)
Howell, Kathleen C.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
February 12, 2019
Publication Date
January 13, 2019
Subject Category
Astrodynamics
Report/Patent Number
JSC-E-DAA-TN64520
Report Number: JSC-E-DAA-TN64520
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Ka''anapali, HI
Country: United States
Start Date: January 13, 2019
End Date: January 17, 2019
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: NNJ13HA01C
CONTRACT_GRANT: HQ NAC TI&E
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
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