Brake Failure from Residual Magnetism in the Mars Exploration Rover Lander Petal Actuator
In January 2004, two Mars Exploration Rover spacecraft arrived at Mars. Each safely delivered an identical rover to the Martian surface in a tetrahedral lander encased in airbags. Upon landing, the airbags deflated and three Lander Petal Actuators opened the three deployable Lander side petals enabling the rover to exit the Lander. Approximately nine weeks prior to the scheduled launch of the first spacecraft, one of these mission-critical Lander Petal Actuators exhibited a brake stuck-open failure during its final flight stow at Kennedy Space Center. Residual magnetism was the definitive conclusion from the failure investigation. Although residual magnetism was recognized as an issue in the design, the lack of an appropriately specified lower bound on brake drop-out voltage inhibited the discovery of this problem earlier in the program. In addition, the brakes had more unit-to-unit variation in drop-out voltage than expected, likely due to a larger than expected variation in the magnetic properties of the 15-5 PH stainless steel brake plates. Failure analysis and subsequent rework of two other Lander Petal Actuators with marginal brakes was completed in three weeks, causing no impact to the launch date.
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