Light Utility Rover

American manned lunar rover. Study 1990. In 1990, Boeing Advanced Civil Space Systems performed an Advanced Civil Space Systems Piloted Rover Technology Assessment Study, which considered both a large pressurized and a small unpressurized rover.

The smaller, Light Utility Rover, would provide 8 hours life support for 2 crew members.

It was designed to transport the crew plus 200 kg of equipment or 300 kg of bulk materials, and perform other light construction and hauling tasks. It had a mass of 984 kg, a length of 4.06 m, and a width of 2.34 m. It was designed for a ground clearance of 0.47 m. Total power was 1 kW, with motors in each drive wheel. Power was supplied by either rechargeable batteries or fuel cells.

Crew Size: 2. Electric System: 1.00 average kW.