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ESA Document - Emits - ESA

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6 APPENDIX A - MARTIAN SURFACE NUCLEAR REACTOR<br />

HMM<br />

Assessment Study<br />

Report: CDF-20(A)<br />

February 2004<br />

page 403 of 422<br />

In the frame of the present study, the option of using a nuclear fission reactor to provide power<br />

for the surface operations was considered in an early stage of the analysis. The design of the<br />

reactor was primarily based on recent European space reactor studies.<br />

Given the short surface stay of the proposed mission and the general conservative approach<br />

chosen, the reactor option was considered not appropriate and is given here for completeness<br />

sake and in the light of further studies involving longer surface stay times.<br />

6.1 General parameters and initial assumptions<br />

It is assumed that the nuclear fission reactor<br />

• serves (only) to deliver electrical power;<br />

• delivers 50 kWe (nominal);<br />

• has a lifetime of about 10 years (minimum of 6 years at operational power);<br />

• complies with international legal standards (especially 1992 UN COPUOS principles and<br />

ICRP recommendations) in terms of operations, safety and radiation protection;<br />

• is activated only after installation on the Martian surface (apart from zero-power testing<br />

on Earth), (no operation during cruise);<br />

• only one reactor is delivered – no system level redundancy.<br />

As regards the total surface power of 50 kWe, note that the final power need of the surface stay<br />

of the current mission scenario is only 3500 Wh/day, which corresponds to an average of 145W.<br />

The power level of 50 kWe for the reactor assessment was made earlier and was maintained<br />

essentially due to two reasons: there is a certain minimum power level for fission reactor systems<br />

to become interesting in terms of specific power, furthermore, fission reactor power systems as<br />

not scale linearly with the power levels provided and even strong decreases of the power need<br />

might not change the total power system mass significantly.<br />

6.2 Reactor type, mass and sizing aspects<br />

6.2.1 General parameters<br />

Compared to terrestrial and naval nuclear reactors, space reactors are orders of magnitude<br />

smaller, in size as well as in power. While the basic principles remain identical – nuclear core<br />

sustaining the controlled chain reaction, heat transport system, electricity generation from heat –<br />

some subsystems are significantly different: waste heat rejection system (e.g. absence of<br />

abundant water), natural coolant/moderator fluent circulation due to gravity, emergency systems<br />

based on gravity.<br />

6.2.2 Main differences to terrestrial systems

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