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Flight Dynamics Analysis of Lunar Fly-By Altitudes and Near Rectilinear Halo Orbit (NRHO) Resonances With Applications to NASA's Artemis ProgramAs the interest in lunar exploration grows exponentially, many companies and government agencies around the world are looking to establish presence on the lunar surface. With NASA’s Artemis program and Lunar Gateway, NASA seeks to return to the moon and for exploration. To achieve such goals, many orbit regimes and patterns were explored. Due to its minimal station keeping requirements and communications access, a specific set of Halo Orbits known as Near Rectilinear Halo Orbits (NRHO) was selected for use cases in both NASA’s Artemis Program as well as Lunar Gateway. The primary objective of this effort is to perform a flight dynamics analysis, which analyzes trajectories targeting specific lunar fly-by altitudes and NRHO Resonances in the L2 Southern Family.
Document ID
20240010205
Acquisition Source
Ames Research Center
Document Type
Poster
Authors
Shazaib Lalani
(University of California, Berkeley Berkeley, United States)
Date Acquired
August 7, 2024
Subject Category
Astrodynamics
Meeting Information
Meeting: NASA Ames Poster Session
Location: Moffet Field, CA
Country: US
Start Date: August 7, 2024
Sponsors: Ames Research Center
Funding Number(s)
OTHER: AL-60687
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
NASA
Spaceflight
Near Rectilinear Halo Orbit
NRHO
Lunar Fly-By
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