The Mars Hopper: An Impulse-Driven, Long-Range, Long-Lived Mobile Platform Utilizing In Situ Martian Resources

Author:

Howe S D1,O'Brien R C2,Ambrosi R M2,Gross B1,Katalenich J1,Sailer L1,Webb J1,McKay M1,Bridges J C2,Bannister N P2

Affiliation:

1. Center for Space Nuclear Research, Idaho Falls, Idaho, USA

2. University of Leicester, Department of Physics and Astronomy, Leicester, UK

Abstract

The requirements for performance by planetary exploration missions are increasing. Landing at a single location to take data is no longer sufficient. Due to the increasing cost, the missions that provide mobile platforms that can acquire data at displaced locations are becoming more attractive. Landers have also had limited range due to power limitations, limited lifetime of subsystems, and the inability to negotiate rough terrain. The Center for Space Nuclear Research has designed an instrumented platform that can acquire detailed data at hundreds of locations during its lifetime — a Mars Hopper. The Mars Hopper concept utilizes energy from radioisotopic decay in a manner different from any existing radioisotopic power source — as a thermal capacitor. By accumulating the heat from radioisotopic decay for long periods, though, the power of the source can be dramatically increased for short periods. Thus, a radioisotopic thermal rocket is possible. The platform will be able to ‘hop’ from one location to the next every 2—3 days with a separation of 10—20km per hop. Each platform will weigh around 50kg unfuelled which is the condition at deployment. Consequently, several platforms may be deployed on a single launch from Earth. With a lifetime estimated at 10 years, the entire surface of Mars can be mapped in detail by a couple dozen platforms. In addition, hoppers can collect samples and deliver them to the Mars Science Laboratory for more detailed analysis. Furthermore, the basic platform can be deployed to Europa, Titan, and even Venus with alterations — the propulsion system and operations essentially will be the same.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Desensitized optimal trajectory for hopping rovers on small bodies;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-06-21

2. The Brahmavarta Initiative: A Roadmap for the First Self-Sustaining City-State on Mars;Universe;2022-10-23

3. Mosquitoes modulate leg dynamics at takeoff to accommodate surface roughness;Bioinspiration & Biomimetics;2018-11-27

4. Analysis of a Radioisotope Thermal Rocket Engine;55th AIAA Aerospace Sciences Meeting;2017-01-05

5. Planetary Robotic System Design;Contemporary Planetary Robotics;2016-08-12

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