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Mars Helicopter Technology DemonstratorAerial exploration of Mars with helicopters could provide mission capabilities that go beyond that of orbiting satellites, landed spacecraft and rovers. Helicopters allow examination of Mars at visual resolutions comparable to landers and rovers but over much longer ranges. They could access and land at designated targets in a controlled manner and could be used to carry or retrieve small payloads. Helicopters could enhance rover missions by quickly scouting out safe traverse routes or providing reconnaissance on possible science target destinations and, as standalone systems, could be used to explore areas that may not be reachable by rovers. Mars helicopters may also be considered as elements of a sample return architecture where they could be used for timely retrieval of small science samples back to a Mars ascent vehicle for return to Earth. The challenge to helicopter use on Mars is the thin carbon dioxide atmosphere with approximately 1% of the density of Earth’s atmosphere. Much like the Sojourner rover on the Pathfinder mission paved the way for the Spirit, Opportunity, Curiosity and the Mars 2020 rovers, an initial demonstration on Mars is desirable so as to inform the development of future helicopter missions. The Jet Propulsion Laboratory is leading a collaborative effort with AeroVironment Inc., and NASA centers Ames, Langley and Glenn to develop a small helicopter as a technology demonstrator. In this paper we briefly describe the results of this effort including results from controlled free-flight of a full-scale (approx 850 g) prototype flown in a test chamber under Mars conditions, the design and development of the 1800 g (not-to-exceed mass) technology demonstrator helicopter, and the operation of the helicopter.
Document ID
20190026832
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Balaram, J. (Bob)
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Canham, Timothy
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Duncan, Courtney
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Golombek, Matt
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Grip, Havard
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Maki, Justin
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Quon, Amelia
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Stern, Ryan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Zhu, David
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Johnson, Wayne
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
July 1, 2019
Publication Date
January 8, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
JPL-CL-CL#17-6243
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition (AIAA SciTech 2018)
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Other

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