Mars Excursion Module


The Mars Excursion Module was a spacecraft proposed by NASA in the 1960s for use in a human mission to Mars, and this can refer to any number of studies by corporations and spaceflight centers for Mars landers. However, primarily a MEM referred to a combination a Manned Mars lander, short-stay surface habitat, and Mars ascent stage. Variations on a MEM included spacecraft designs like an unmanned Mars surface cargo delivery, and there was a MEM lander that combined a communications center, living habitat, and laboratory.
A MEM formed part of Mars orbit rendezvous and flyby-rendezvous mission profiles studied at NASA's Manned Spacecraft Center in the 1960s. A Mars Excursion Module would have been a combination of a Mars lander, short-stay surface habitat, and ascent vehicle; the ascent stage performed the rendezvous. One design for a MEM would have been used for a 40-day stay on the Martian surface in the flyby-rendezvous mission profile or for a 10- to 40-day stay in the MOR profiles. There was also a descent-only uncrewed MEM for delivering cargo, like a rover to the surface of Mars. Another MEM cargo lander variant would deliver a nuclear reactor to support the surface operations, and there was another with a communications, living quarters and lab in one landing-only MEM unit.
In the early 1960s, NASA contracted Philco Corporation to design a Mars Excursion Module for a Mars mission for the early 1970s. The basic requirements were for a crew of two, one US ton of science hardware, and to support 40 days of surface operation on Mars. Another MEM from this period was the Ames contracted TRW MEM, a design which weighed 11.4 metric tons but was designed for Mars atmosphere which had 10% of Earth's.
The watershed moment for mission planning was July 1965, when Mariner IV returned more accurate atmospheric data about Mars. This ruled out many of the lifting body and glider designs that were being considered based on estimates of a thicker Mars atmosphere than revealed by Mariner IV.
Gordon Woodcock at the NASA Marshal Space Flight Center worked on the basis of a thinner Mars atmosphere, and developed design for a MEM, and also a pure-lander variant that would deliver a pressurized manned Mars rover called Molab.

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