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Main Authors: Yu, Wayne, Williams, Trevor, Carpenter, Russell
Format: Preprint
Published: 2025
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Online Access:https://arxiv.org/abs/2505.15732
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author Yu, Wayne
Williams, Trevor
Carpenter, Russell
author_facet Yu, Wayne
Williams, Trevor
Carpenter, Russell
contents The Fermi Gamma ray Space Telescope, launched in 2008, has over 16 years of operations providing gamma ray (8 keV to 300 Gev) spectra science observations of cosmic phenomena. It continues to provide invaluable research for the astrophysics community which include the study of pulsars, cosmic rays, gamma ray bursts, and coordination with gravity wave observations for neutron star mergers. The Fermi Earth orbit at a 500 x 512 km altitude is subject to collision warnings due to new constellations deployed near Fermi: currently over 7,000 satellites and growing. This paper presents analysis concerning changing Fermi's orbit and associated operational flight dynamics considerations. The cadence of burns and expected fuel use for a proposed orbit raise scenario is examined, ensuring that Fermi should have sufficient fuel for end of life operations. In addition, a Monte Carlo design is presented to capture single maneuver model uncertainty.
format Preprint
id arxiv_https___arxiv_org_abs_2505_15732
institution arXiv
publishDate 2025
record_format arxiv
spellingShingle Designing a Potential NASA Fermi Orbit Change
Yu, Wayne
Williams, Trevor
Carpenter, Russell
Earth and Planetary Astrophysics
High Energy Astrophysical Phenomena
Instrumentation and Methods for Astrophysics
The Fermi Gamma ray Space Telescope, launched in 2008, has over 16 years of operations providing gamma ray (8 keV to 300 Gev) spectra science observations of cosmic phenomena. It continues to provide invaluable research for the astrophysics community which include the study of pulsars, cosmic rays, gamma ray bursts, and coordination with gravity wave observations for neutron star mergers. The Fermi Earth orbit at a 500 x 512 km altitude is subject to collision warnings due to new constellations deployed near Fermi: currently over 7,000 satellites and growing. This paper presents analysis concerning changing Fermi's orbit and associated operational flight dynamics considerations. The cadence of burns and expected fuel use for a proposed orbit raise scenario is examined, ensuring that Fermi should have sufficient fuel for end of life operations. In addition, a Monte Carlo design is presented to capture single maneuver model uncertainty.
title Designing a Potential NASA Fermi Orbit Change
topic Earth and Planetary Astrophysics
High Energy Astrophysical Phenomena
Instrumentation and Methods for Astrophysics
url https://arxiv.org/abs/2505.15732