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Space Mission Options for Reconnaissance and Mitigation of Asteroid 2024 YR4Near-Earth asteroid 2024 YR4 was discovered on 2024-12-27 and its probability of Earth impact in December 2032 peaked at ∼3% on 2025-02-18. Additional observations ruled out Earth impact by 2025-02-23. However, the probability of lunar impact in December 2032 then rose, reaching ∼4% by the end of the apparition in May 2025. James Webb Space Telescope (JWST) observations on 2025-03-26 estimated the asteroid’s diameter at 60 ± 7 m. Studies of 2024 YR4’s potential lunar impact effects suggest lunar ejecta could increase micrometeoroid debris flux in low Earth orbit up to 1000 times above background levels over just a few days, possibly threatening astronauts and spacecraft. In this work, we present options for space missions to 2024 YR4 that could be utilized if lunar impact is confirmed. We cover flyby & rendezvous reconnaissance, deflection, and robust disruption of the asteroid. We examine both rapid-response and delayed launch options through 2032. We evaluate chemical and solar electric propulsion, various launch vehicles, optimized deep space maneuvers, and gravity assists. Re-tasking extant spacecraft and using built spacecraft not yet launched are also considered. The best reconnaissance mission options launch in late 2028, leaving only approximately three years for development at the time of this writing in August 2025. Deflection missions were assessed and appear impractical. However, kinetic robust disruption missions are available with launches between April 2030 and April 2032. Nuclear robust disruption missions are also available with launches between late 2029 and late 2031. Finally, even if lunar impact is ruled out there is significant potential utility in deploying a reconnaissance mission to characterize the asteroid.
Document ID
20250008941
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Brent W Barbee
(Goddard Space Flight Center Greenbelt, United States)
Matthew A Vavrina
(AI Solutions Lanham, Maryland, United States)
Rylie Bull
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
Adrienne Rudolph
(University of Maryland, College Park College Park, United States)
Davide Farnocchia
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Russell TerBeek
(Sandia National Laboratories California Livermore, United States)
Justin Atchison
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
Joshua Lyzhoft
(Goddard Space Flight Center Greenbelt, United States)
Jessie Dotson
(Ames Research Center Mountain View, United States)
Patrick King
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
Paul W Chodas
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Dawn Graninger
(Johns Hopkins University Applied Physics Laboratory North Laurel, United States)
Ronald G Mink
(Goddard Space Flight Center Greenbelt, United States)
Kathryn M Kumamoto
(Lawrence Livermore National Laboratory Livermore, United States)
Jason M Pearl
(Lawrence Livermore National Laboratory Livermore, United States)
Mary Burkey
(Lawrence Livermore National Laboratory Livermore, United States)
Isaiah Santistevan
(Lawrence Livermore National Laboratory Livermore, United States)
Catherine S Plesko
(Los Alamos National Laboratory Los Alamos, United States)
Wendy K Caldwell
(Los Alamos National Laboratory Los Alamos, United States)
Megan Harwell
(Los Alamos National Laboratory Los Alamos, United States)
Date Acquired
September 3, 2025
Publication Date
September 3, 2025
Publication Information
Publication: The Journal of the Astronautical Sciences
Publisher: Springer
ISSN: 0021-9142
e-ISSN: 2195-0571
Subject Category
Astrodynamics
Lunar and Planetary Science and Exploration
Astronomy
Funding Number(s)
CONTRACT_GRANT: 80NM0018D0004
WBS: 582622.02.01.04.66
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Asteroid Deflection
Asteroid Disruption
Trajectory Optimization
Planetary Defense
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