Research Project

Mars Science Helicopter: Mass Optimization

Research Team

Lead Researchers:

  • Prof. Amiel Hartman, Mechanical Engineering
  • Dr. Bingbing Li, Manufacturing Systems Engineering
  • Dr. Ashley Geng, Electrical and Computer Engineering

Collaborators:

  • Dr. Greg Agnes
  • Dr. Larry Matthies

Student Team:

  • Jared Carrillo
  • Benjamin Sun
  • Elliott Sadler
  • Marshall Doyle
  • Phanichandra Mylavarapu

Funding

  • Funding Organization:
  • Funding Program:

SYNOPSIS

Design elements to optimize mass requirements for the Mars Science Helicopter

  • Mission Requirements
    • Operate under specific temperature ranges, survive launch forces,
      7-minute flight time, 30 m/s flight speed
  • Design Criteria
    • ~4 Meter Diameter (with arms) and ~1 Meter Diameter (Chassis)
    • 18kg mass and payload mass of 2kg
    • Foldable Design
Mars Science Helicopter Project Image Collage of Prototype/Design Concepts
Research Questions and Research Objectives
  • Develop a Mars helicopter chassis optimized for

    • Mass

    • Vibrational Forces

    • Thermal Issues

  • Develop with new manufacturing concepts such as

    • Generative Design

    • Metal 3D Printing

    • Carbon Fiber

  • Validate design through digital twin simulations

    • Omniverse

    • Ansys

Research Methods
  • Use generative design to create lightweight, efficient drone structures for enhanced performance and rapid design iterations.

  • Apply thermal optimization through custom CFD API for Fusion 360 to ensure the mechanical structure withstands extreme temperature fluctuations during the mission.

  • Utilize finite element analysis to address mechanical and vibrational issues, ensuring system robustness in demanding environments.

Research Results and Deliverables
  • Derived JPL Design Requirements

    • Chassis Size Range

    • Max Weight

  • Finished standard chassis design and optimization as a reference point for testing against generative design iterations

    • Isogrid Design

    • Tube Truss Design

Commercialization Opportunities
  • Application: Decrease spacecraft iteration time and cost

  • Key Values: Generative design, optimization, analysis

  • Potential Customers: Space industry, automotive industry

Research Timeline

Start Date:
End Date:

Research Team

Lead Researchers:

  • Prof. Amiel Hartman, Mechanical Engineering
  • Dr. Bingbing Li, Manufacturing Systems Engineering
  • Dr. Ashley Geng, Electrical and Computer Engineering

Collaborators:

  • Dr. Greg Agnes
  • Dr. Larry Matthies

Student Team:

  • Jared Carrillo
  • Benjamin Sun
  • Elliott Sadler
  • Marshall Doyle
  • Phanichandra Mylavarapu

Funding

  • Funding Organization:
  • Funding Program: