United States planetary rover status: 1989
A spectrum of concepts for planetary rovers and rover missions, is covered. Rovers studied range from tiny micro rovers to large and highly automated vehicles capable of traveling hundreds of kilometers and performing complex tasks. Rover concepts are addressed both for the Moon and Mars, including a Lunar/Mars common rover capable of supporting either program with relatively small modifications. Mission requirements considered include both Science and Human Exploration. Studies include a range of autonomy in rovers, from interactive teleoperated systems to those requiring and onboard System Executive making very high level decisions. Both high and low technology rover options are addressed. Subsystems are described for a representative selection of these rovers, including: Mobility, Sample Acquisition, Science, Vehicle Control, Thermal Control, Local Navigation, Computation and Communications. System descriptions of rover concepts include diagrams, technology levels, system characteristics, and performance measurement in terms of distance covered, samples collected, and area surveyed for specific representative missions. Rover development schedules and costs are addressed for Lunar and Mars exploration initiatives.
Related Mars Exploration Documents
1999 Marsokhod Field Experiment: A Simulation of a Mars Rover Science Mission
A field experiment to simulate a rover mission to Mars was performed in February 1999. This experiment, the latest in a series of rover field experiments, was designed to demonstrate and validate tech
A Compact Tensegrity Lander and Rover Concept for Exploration of Martian Terrains
The proposed concept is a redesign of the Tension Adjustable Network for Deploying Entry Membrane (TANDEM) tensegrity rover for a low-cost mission to Mars. Focus is on the entry, descent, landing, and
A conceptual design and operational characteristics for a Mars rover for a 1979 or 1981 Viking science mission
The feasibility of a small Mars rover for use on a 1979 or 1981 Viking mission was studied and a preliminary design concept was developed. Three variations of the concept were developed to provide com