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Sensitivity of the Asteroid Redirect Robotic Mission (ARRM) to Launch Date and Asteroid Stay TimeNational Aeronautics and Space Administrations (NASAs) proposed Asteroid Redirect Mission (ARM) is being designed to robotically capture and then redirect an asteroidal boulder mass into a stable orbit in the vicinity of the moon, where astronauts would be able to visit and study it. The current reference trajectory for the robotic portion, ARRM, assumes a launch on a Delta IV H in the end of the calendar year 2021, with a return for astronaut operations in cislunar space in 2026. The current baseline design allocates 245 days of stay time at the asteroid for operations and boulder collection. This paper outlines analysis completed by the ARRM mission design team to understand the sensitivity of the reference trajectory to launch date and asteroid stay time.
Document ID
20170007299
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Mcguire, Melissa L.
(NASA Glenn Research Center Cleveland, OH United States)
Burke, Laura M.
(NASA Glenn Research Center Cleveland, OH United States)
McCarty, Steven L.
(NASA Glenn Research Center Cleveland, OH United States)
Strange, Nathan J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Qu, Min
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Shen, Haijun
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Vavrina, Matthew A.
(AI Solutions, Inc. Lanham, MD, United States)
Date Acquired
August 3, 2017
Publication Date
February 5, 2017
Subject Category
Astrodynamics
Report/Patent Number
GRC-E-DAA-TN38898
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: San Antonio, TX
Country: United States
Start Date: February 5, 2017
End Date: February 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: WBS 466159.02.12.05.01
CONTRACT_GRANT: NNL12AA09C
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
trajectory analysis
trajectory optimization
spacecraft trajectories
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