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An Advanced Mars Helicopter DesignIngenuity may be the first of many Mars aerial vehicles. Rotorcraft increase the range and speed that can be traveled to locations of interest. This enables mission concepts previously considered not viable on Mars, such as missions performing science investigations in regions of high elevation, steep terrain, caves/lava tubes, and surveys of the lower atmosphere. Recent work done at NASA Ames Research Center and NASA’s Jet Propulsion Laboratory (JPL) show that significant science can be performed by rotorcraft either independently or as assistants to rovers and landers. Small rotorcraft of Ingenuity’s general size can be potentially integrated into missions already scheduled for launch. Additionally, larger rotorcraft can support standalone novel mission concepts but are still be able to be sized and configured for deployment from heritage entry, descent, and landing (EDL) systems. One such mission concept of interest is to determine if organics are associated with clay-bearing or silica-rich soil. For such a mission, a small rotorcraft “robotic assistant” to a lander or rover could help determine if ancient sediment contains biosignatures in regions such as Mawrth Vallis. Ingenuity has demonstrated that rotorcraft can be developed relatively quickly and inexpensively and increase the types and amount of science that can be performed on any given mission. Recent research has suggested that rotorcraft of Ingenuity’s general size can have their performance characteristics significantly enhanced – increasing their range, speed, and payload capacity – by using new generation rotor blade airfoils optimized for Mars operating conditions. Rotorcraft could potentially be a standard adjunct to all future lander and rover missions. This paper presents an advanced Mars helicopter design that leverages significantly the design heritage of the Ingenuity Mars Helicopter Technology Demonstrator (MHTD).
Document ID
20205008553
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Shannah Withrow-Maser
(Ames Research Center Mountain View, California, United States)
Wayne Johnson
(Ames Research Center Mountain View, California, United States)
Larry Young
(Ames Research Center Mountain View, California, United States)
Haley Cummings
(Ames Research Center Mountain View, California, United States)
Athena Chan
(Science and Technology Corporation (United States) Hampton, Virginia, United States)
Theodore Tzanetos
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
J Balaram
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Jonathan Bapst
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
October 12, 2020
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA ASCEND
Location: Online
Country: US
Start Date: November 16, 2020
End Date: November 18, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 664817
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Advanced
Mars Helicopter
Design
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