DRM MAV Ascent Credit - NASA

The first version of the NASA Cargo Lander for the design reference mission would land an Earth Entry/Mars Ascent Capsule, an ascent stage, and an ISRU plant on the surface that would produce propellant for the crew's return journey from the Martian atmosphere. It had a typical mass of 90,190 kg on approach to Mars and 60,920 kg on the surface.

Cargo Lander 1 Reference Version 1.0 Mass Summary Earth Entry/Mars Ascent Capsule: 5,500 kg Ascent stage dry mass: 2,550 kg ISRU plant: 4,802 kg Hydrogen feedstock: 4,500 kg PVA keep-alive power system: 300 kg 160 kw nuclear power plant: 12,498 kg 1.0 km power cables, PMAD: 1,900 kg Communication system: 820 kg Pressurized Rover: 15,500 kg 15 kwe DIPS cart: 1,100 kg Unpressurized rover: 440 kg 3 teleoperable science rovers: 1,320 kg Water storage tank: 1,220 kg Science equipment: 3,800 kg TOTAL CARGO MASS: 56,250 kg Terminal propulsion system: 4,670 kg TOTAL LANDED MASS: 60,920 kg Propellant: 11,970 kg Forward Aeroshell: 17,300 kg TOTAL ENTRY MASS: 90,190 kg NTR Propulsion System: 28,900 TMI Propellant: 86,000 kg TOTAL INITIAL MASS: 205,090 kg

Length: 40.30 m (132.20 ft). Mass: 205,090 kg (452,140 lb).