Critical Aerodynamic and Performance Upgrades to Enable Larger Mars Rotorcraft Such as the Chopper Platform

Leveraging lessons learned from NASA's Ingenuity Mars helicopter and concepts such as the Mars Sample Recovery Helicopter, and Mars Science Helicopter has enabled partners at NASA's Jet Propulsion Laboratory (JPL), NASA Ames, and AeroVironment, Inc. to mature a hexacopter vehicle concept (Chopper) with the ability to support a wide range of mission scenarios. This work focuses on the critical aeronautics-related challenges encountered transitioning from an Ingenuity-size vehicle to a much larger vehicle (˜15 times the mass) and discusses engineering efforts to address these challenges. Critical upgrades include optimized airfoils, higher solidity blades, and higher fidelity computational models. Because multiple rotors are required to lift the heavier vehicle, increased understanding of the impact of rotor-to-rotor interactions is also necessary. Rotors have been designed that are tailored to more demanding missions and will be validated in a joint test campaign between the partners. While the Chopper concept will be utilized to illustrate these maturation efforts, the lessons learned are applicable to other heavier next generation Mars rotorcraft platforms also.

Authors

Publication Details

Published
2025-05-20
DOI
https://doi.org/10.4050/f-0081-2025-388
Citations
2
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
9.99
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article

Critical Aerodynamic and Performance Upgrades to Enable Larger Mars Rotorcraft Such as the Chopper Platform

Carlos Malpica, Laura Jones-Wilson, Wayne Johnson, Shannah Withrow-Maser et al.
2 citations
Spacecraft Dynamics and Control
9.99
article

Critical Aerodynamic and Performance Upgrades to Enable Larger Mars Rotorcraft Such as the Chopper Platform

Carlos Malpica, Laura Jones-Wilson, Wayne Johnson, Shannah Withrow-Maser, Marcel Veismann, Witold J. F. Koning, Fernando Mier-Hicks, Allen Ruan, Gianmarco Sahragard-Monfared, Joshua P. Bowman, Jeff Delaune, Jacob Izraelevitz, Dorcas Kaweesa, Tove Aagren, Kimberly Dana Ainza Sneeder
article en
2 citations

Abstract

Leveraging lessons learned from NASA's Ingenuity Mars helicopter and concepts such as the Mars Sample Recovery Helicopter, and Mars Science Helicopter has enabled partners at NASA's Jet Propulsion Laboratory (JPL), NASA Ames, and AeroVironment, Inc. to mature a hexacopter vehicle concept (Chopper) with the ability to support a wide range of mission scenarios. This work focuses on the critical aeronautics-related challenges encountered transitioning from an Ingenuity-size vehicle to a much larger vehicle (˜15 times the mass) and discusses engineering efforts to address these challenges. Critical upgrades include optimized airfoils, higher solidity blades, and higher fidelity computational models. Because multiple rotors are required to lift the heavier vehicle, increased understanding of the impact of rotor-to-rotor interactions is also necessary. Rotors have been designed that are tailored to more demanding missions and will be validated in a joint test campaign between the partners. While the Chopper concept will be utilized to illustrate these maturation efforts, the lessons learned are applicable to other heavier next generation Mars rotorcraft platforms also.

Openalex Percentile: Top 3%
Spacecraft Dynamics and Control
9.99
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Critical Aerodynamic and Performance Upgrades to Enable Larger Mars Rotorcraft Such as the Chopper Platform — Carlos Malpica, Laura Jones-Wilson, et al. · (2025) | TGRS Research Map | TGRS