AEOLUS: A System Concept for Precise Delivery of Mars Scientific Instrumentation

The AEOLUS system concept is proposed to deliver science instruments with great precision to the surface of Mars. This capability is regarded as an important next step in bringing Mars evolutionary processes into greater focus by allowing investigation of specifically targeted sites. By the use of existing maneuvering vehicle technology, terrain guidance hardware, and other vehicle subsystems this mission appears feasible with a minimum amount of development and risk. The conceptual system design presented in this paper is capable of delivering a variety of instrumentation types (the first phase is a penetrator/flight experiment, followed by a rover mission) with 3 sigma accuracies of approximately 1 km compared with the typical Mars Pathfinder landing ellipse of 150 km. This allows the utility of small rovers to greatly increase as the goal is to develop a system such that the rover range exceeds the landing ellipse of the delivery system. The proposed mission using available technologies in combination with a novel approach to transportation, results in attractive mission costs from $35M-$50M. The system name "AEOLUS" (Greek god of the air and wind) was chosen since it would represent controlled flight in another planetary atmosphere.

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Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-08-21
DOI
https://doi.org/10.26077/9pbs-d387
Primary Topic
Planetary Science and Exploration
Type
article

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article

AEOLUS: A System Concept for Precise Delivery of Mars Scientific Instrumentation

David Keese, Marcus Murbach, Jack D. Farmer
Digital Commons - USU (Utah State University)
Planetary Science and Exploration
article

AEOLUS: A System Concept for Precise Delivery of Mars Scientific Instrumentation

David Keese, Marcus Murbach, Jack D. Farmer
article en

Abstract

The AEOLUS system concept is proposed to deliver science instruments with great precision to the surface of Mars. This capability is regarded as an important next step in bringing Mars evolutionary processes into greater focus by allowing investigation of specifically targeted sites. By the use of existing maneuvering vehicle technology, terrain guidance hardware, and other vehicle subsystems this mission appears feasible with a minimum amount of development and risk. The conceptual system design presented in this paper is capable of delivering a variety of instrumentation types (the first phase is a penetrator/flight experiment, followed by a rover mission) with 3 sigma accuracies of approximately 1 km compared with the typical Mars Pathfinder landing ellipse of 150 km. This allows the utility of small rovers to greatly increase as the goal is to develop a system such that the rover range exceeds the landing ellipse of the delivery system. The proposed mission using available technologies in combination with a novel approach to transportation, results in attractive mission costs from $35M-$50M. The system name "AEOLUS" (Greek god of the air and wind) was chosen since it would represent controlled flight in another planetary atmosphere.

Digital Commons - USU (Utah State University)
Ames Research Center (US), Sandia National Laboratories (US)
National Aeronautics and Space Administration, Goddard Space Flight Center, Sandia National Laboratories
Planetary Science and Exploration
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AEOLUS: A System Concept for Precise Delivery of Mars Scientific Instrumentation — David Keese, Marcus Murbach, et al. · Digital Commons - USU (Utah State University) (2025) | TGRS Research Map | TGRS