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Innovative Offloading of Astronauts for More Effective Exploration

David Akin
University of Maryland, College Park

BioBot on planetary surface.
Graphic depiction of BioBot: Innovative Offloading of Astronauts for More Effective Exploration. Credits: David Akin

No parameter in the design of spacesuits for planetary exploration is more important than ‘weight on the back’- the weight of the suit system which must be supported by the wearer under the gravity of the Moon or Mars. The added weight of the spacesuit garment and portable life support system (PLSS) drives the required exertion level of the wearer, and ultimately sets limitations on EVA duration, distance traveled on foot, and productivity of the exploration mission.

As an example, the A7L-B suits worn on the later Apollo lunar missions had an Earth weight of 212 lbs, composed of 77 lbs for the garment assembly and 135 lbs for the PLSS. A 160 lb astronaut found their weight increased by 130% due to the suit, with the PLSS weight alone almost equal to his body weight. This system was capable of supporting a 6-hour nominal surface EVA, but strongly impacted the gaits, transport speeds, and energy expenditures of the astronauts. The PLSS weight was particularly burdensome, as it moved the astronaut’s overall center of mass upwards and backwards. This could be seen in the convoluted motions of the crew when trying to bend over and pick up items, work with the long-handled sampling tools, or just maintain balance, especially when changing direction or starting and stopping.
The seminal concept of BioBot is an autonomous robotic system to handle life support umbilicals on planetary surfaces in the vicinity of obstacles and snag hazards. This enables the BioBot system concept, which consists of a robotic rover which is capable of traversing the same terrain as a spacesuited human. It carries the primary life support system for the astronaut, including consumables, atmosphere revitalization systems (e.g., CO2 scrubbing, humidity and temperature management, ventilation fan), power system (e.g., battery, power management and distribution), and thermal control system (e.g., water sublimator, cooling water pump), along with umbilical lines to connect to the supported astronaut via the autonomous umbilical handling system.
Building on the successful concept demonstrations of Phase 1, this proposal focuses on further development of the autonomous umbilical handling system, and on obtaining the most mission-relevant information possible by participating in science field tests at Lava Beds National Monument in northern California. It also proposes to perform testing at the NASA Johnson Space Center to engage NASA subject matter experts in EVA, robotics, and exploration systems.

2020 Phase I, II, and III Selections