An anthropocentric concept of take off and landing system for a Martian expedition

Аuthors

Abstract

Functional requirements are suggested for component parts of take off and landing system intended to a Martian expedition. Corresponding research to make these requirements is carried out basing on preliminary scripts and designs for an interplanetary expedition to land on the Martian surface. One of the main goals of the research consists in providing of efficient extravehicular activity of cosmonauts after a landing on the planet surface.