Mars revolving observation satellite

Computer Science

Scientific paper

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Japanese Spacecraft, Mars Probes, Mission Planning, Satellite Control, Satellite Design, Satellite Orbits, Spacecraft Components, Spacecraft Equipment, Data Systems, Mars (Planet), Orbital Mechanics, Spacecraft Power Supplies, Spacecraft Propulsion, Weight Analysis

Scientific paper

A study concerning the possibility of a Mars revolving satellite, to be launched in the first part of the 21st century, is presented. It is believed that this is a necessary step before proceeding to Mars landings, bases, and further exploration. The mission requirements are as follows: (1) a precision Mars mapping, including topography information; (2) a Mars resources exploration by spectral absorption examination of the Mars surface; (3) a Mars atmospheric investigation; (4) a survey of the Mars polar cap; and (5) a radioactive environment survey. The system structure, electric power and weight analysis, and fuel analysis are presented. A subsystem analyses concerning attitude control, communication, electric power, data processing, and propulsion and reaction control subsystems is also provided.

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