Mars Excursion Module

The Mars Excursion Module (MEM) 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 of a Manned Mars lander, short-stay surface habitat, and Mars ascent stage. Variations on a MEM included spacecraft designs like an uncrewed Mars surface cargo delivery, and there was a MEM lander that combined a communications center, living habitat, and laboratory.[1]

A MEM formed part of Mars orbit rendezvous (MOR) and flyby-rendezvous mission profiles studied at NASA's Manned Spacecraft Center in the 1960s.[2] 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.[2] There was also a descent-only uncrewed MEM for delivering cargo, like a rover to the surface of Mars.[3] 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.[1]

  1. ^ a b Woodcock, G. R. (7 June 1966). "An Initial Concept of a Manned Mars Excursion Vehicle for a Tenuous Mars Atmosphere" (PDF). NASA. Retrieved 22 September 2018.
  2. ^ a b Portree, David S. F. (February 2001). "Chapter 3: Empire and After". Humans to Mars: Fifty Years of Mission Planning, 1950–2000 (PDF). NASA Monographs in Aerospace History Series. National Aeronautics and Space Administration. pp. 15–18. Retrieved 18 July 2014.
  3. ^ "Origin of the Apollo-shaped Manned Mars Lander (1966)". Wired. 25 October 2012. Retrieved 4 March 2018.

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