The Ice Giants may become a sought-after destination in the coming decades as researchers aim to have a better awareness of our Solar system- its origins and growth. The interplanetary trajectory optimization is an important aspect of the analysis of a mission to Uranus. This study investigates possible interplanetary paths to Uranus in the 2022-2030 timeframe. It provides a preliminary estimate of fuel consumption in units of ΔV for various mission durations. A variety of approaches can be used to travel from Earth to another planet. It is conceivable to use a direct transfer route with two engine burns, one at a parking orbit around the Earth and the other to capture around the target planet. This article emphasizes a direct transfer trajectory analysis towards Uranus using Lambert’s problem. Different lambert arcs were considered for the direct transfer. Variations of excess velocities at arrival and departure for various time-of-flight were obtained. The ceiling of the time-of-flight was fixed as 16.5 years by performing a Hohmann transfer. The minimum ΔV was obtained for various time-of-flight ranging from 8.5 years to 16.5 years. The ideal ΔV obtained during the fixed timeframe lies between 6.87 km/s and 7.98 km/s. The minimum value of ΔV was observed for the time-of-flight of 13.5 years.
| Published in | International Journal of Astrophysics and Space Science (Volume 10, Issue 1) |
| DOI | 10.11648/j.ijass.20221001.12 |
| Page(s) | 9-17 |
| Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
| Copyright |
Copyright © The Author(s), 2024. Published by Science Publishing Group |
Direct Transfer Trajectory, Lambert’s Problem, Patched-Conic Method, Earth-Uranus Mission, Optimal Delta-V, Interplanetary Mission
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APA Style
Gisa Geoson Suseela, Yadu Krishnan Sukumarapillai, Hariprasad Thimmegowda, Pavan Kalyan Devaiah, Manjunath Nagendra, et al. (2022). Analysis of Earth-Uranus Direct-Transfer Trajectory for Optimal Delta-V Using Lambert’s Problem. International Journal of Astrophysics and Space Science, 10(1), 9-17. https://doi.org/10.11648/j.ijass.20221001.12
ACS Style
Gisa Geoson Suseela; Yadu Krishnan Sukumarapillai; Hariprasad Thimmegowda; Pavan Kalyan Devaiah; Manjunath Nagendra, et al. Analysis of Earth-Uranus Direct-Transfer Trajectory for Optimal Delta-V Using Lambert’s Problem. Int. J. Astrophys. Space Sci. 2022, 10(1), 9-17. doi: 10.11648/j.ijass.20221001.12
AMA Style
Gisa Geoson Suseela, Yadu Krishnan Sukumarapillai, Hariprasad Thimmegowda, Pavan Kalyan Devaiah, Manjunath Nagendra, et al. Analysis of Earth-Uranus Direct-Transfer Trajectory for Optimal Delta-V Using Lambert’s Problem. Int J Astrophys Space Sci. 2022;10(1):9-17. doi: 10.11648/j.ijass.20221001.12
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Download@article{10.11648/j.ijass.20221001.12,
author = {Gisa Geoson Suseela and Yadu Krishnan Sukumarapillai and Hariprasad Thimmegowda and Pavan Kalyan Devaiah and Manjunath Nagendra and Tamore Silviya Dhiraj},
title = {Analysis of Earth-Uranus Direct-Transfer Trajectory for Optimal Delta-V Using Lambert’s Problem},
journal = {International Journal of Astrophysics and Space Science},
volume = {10},
number = {1},
pages = {9-17},
doi = {10.11648/j.ijass.20221001.12},
url = {https://doi.org/10.11648/j.ijass.20221001.12},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijass.20221001.12},
abstract = {The Ice Giants may become a sought-after destination in the coming decades as researchers aim to have a better awareness of our Solar system- its origins and growth. The interplanetary trajectory optimization is an important aspect of the analysis of a mission to Uranus. This study investigates possible interplanetary paths to Uranus in the 2022-2030 timeframe. It provides a preliminary estimate of fuel consumption in units of ΔV for various mission durations. A variety of approaches can be used to travel from Earth to another planet. It is conceivable to use a direct transfer route with two engine burns, one at a parking orbit around the Earth and the other to capture around the target planet. This article emphasizes a direct transfer trajectory analysis towards Uranus using Lambert’s problem. Different lambert arcs were considered for the direct transfer. Variations of excess velocities at arrival and departure for various time-of-flight were obtained. The ceiling of the time-of-flight was fixed as 16.5 years by performing a Hohmann transfer. The minimum ΔV was obtained for various time-of-flight ranging from 8.5 years to 16.5 years. The ideal ΔV obtained during the fixed timeframe lies between 6.87 km/s and 7.98 km/s. The minimum value of ΔV was observed for the time-of-flight of 13.5 years.},
year = {2022}
}
TY - JOUR T1 - Analysis of Earth-Uranus Direct-Transfer Trajectory for Optimal Delta-V Using Lambert’s Problem AU - Gisa Geoson Suseela AU - Yadu Krishnan Sukumarapillai AU - Hariprasad Thimmegowda AU - Pavan Kalyan Devaiah AU - Manjunath Nagendra AU - Tamore Silviya Dhiraj Y1 - 2022/06/21 PY - 2022 N1 - https://doi.org/10.11648/j.ijass.20221001.12 DO - 10.11648/j.ijass.20221001.12 T2 - International Journal of Astrophysics and Space Science JF - International Journal of Astrophysics and Space Science JO - International Journal of Astrophysics and Space Science SP - 9 EP - 17 PB - Science Publishing Group SN - 2376-7022 UR - https://doi.org/10.11648/j.ijass.20221001.12 AB - The Ice Giants may become a sought-after destination in the coming decades as researchers aim to have a better awareness of our Solar system- its origins and growth. The interplanetary trajectory optimization is an important aspect of the analysis of a mission to Uranus. This study investigates possible interplanetary paths to Uranus in the 2022-2030 timeframe. It provides a preliminary estimate of fuel consumption in units of ΔV for various mission durations. A variety of approaches can be used to travel from Earth to another planet. It is conceivable to use a direct transfer route with two engine burns, one at a parking orbit around the Earth and the other to capture around the target planet. This article emphasizes a direct transfer trajectory analysis towards Uranus using Lambert’s problem. Different lambert arcs were considered for the direct transfer. Variations of excess velocities at arrival and departure for various time-of-flight were obtained. The ceiling of the time-of-flight was fixed as 16.5 years by performing a Hohmann transfer. The minimum ΔV was obtained for various time-of-flight ranging from 8.5 years to 16.5 years. The ideal ΔV obtained during the fixed timeframe lies between 6.87 km/s and 7.98 km/s. The minimum value of ΔV was observed for the time-of-flight of 13.5 years. VL - 10 IS - 1 ER -
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