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
- Carlos Malpica
- Laura Jones-Wilson (ORCID: https://orcid.org/0000-0002-3675-5419)
- Wayne Johnson (ORCID: https://orcid.org/0000-0003-4280-5715)
- Shannah Withrow-Maser
- Marcel Veismann (ORCID: https://orcid.org/0000-0001-8106-6738)
- Witold J. F. Koning
- Fernando Mier-Hicks
- Allen Ruan
- Gianmarco Sahragard-Monfared (ORCID: https://orcid.org/0000-0002-6527-7380)
- Joshua P. Bowman (ORCID: https://orcid.org/0000-0002-7705-3069)
- Jeff Delaune (ORCID: https://orcid.org/0000-0003-1509-4401)
- Jacob Izraelevitz
- Dorcas Kaweesa
- Tove Aagren
- Kimberly Dana Ainza Sneeder
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