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ESA Document - Emits - ESA

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1 INTRODUCTION<br />

1.1 Background<br />

HMM<br />

Assessment Study<br />

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

February 2004<br />

page 19 of 422<br />

In November 2001, the <strong>ESA</strong> Council at Ministerial level approved the Aurora Programme<br />

dedicated to the human and robotic exploration of the Moon, Mars and asteroids. The ultimate<br />

goal of the Aurora Programme is human exploration of Mars foreseen in 2025-2030 time frame.<br />

A first <strong>ESA</strong> activity performed with industrial support concerned high level trades and defined<br />

some of the mission boundaries and constraints.<br />

Subsequently, the Aurora Programme asked for further internal activities to refine and detail the<br />

above trades.<br />

The main objective of the study was not to define an <strong>ESA</strong> “reference human mission to Mars”<br />

but rather to start an iteration cycle which should lead to the definition of the exploration strategy<br />

and the associated missions and the set-up of requirements for further mission design and further<br />

feedback to the exploration plan. The mission shown in the report is a design case, and does not<br />

address prior technology demonstration missions. These are covered separately by the Aurora<br />

Long Term Plan.<br />

Peer reviews of the design case have been performed in ESTEC and reports are available as<br />

separate documents.<br />

1.2 CDF study<br />

Within the time frame September 2003-February 2004, in two phases, for a total of 23 sessions,<br />

the ESTEC Concurrent Design Facility (CDF) performed an assessment study of a Human<br />

Mission to Mars, known as the HMM study.<br />

The results of this study are reported in this document.<br />

1.3 <strong>Document</strong> structure<br />

This document is structured so that the background to the study is described first, followed by an<br />

executive summary that gives an overview of the mission. This is followed by the chapters<br />

introducing the mission analysis and the mission architecture trade-offs.<br />

The actual subsystem designs that were performed in the study were split into two main separate<br />

vehicles: the Transfer Vehicle (TV) and the Mars Excursion Vehicle (MEV). In turn, these two<br />

vehicles are split into their main subvehicles/components.<br />

The document includes the chapters relevant to some other overall disciplines such as operations,<br />

cost, risk, programmatics and simulation.<br />

Due to the different distribution requirements, only the cost assumptions (excluding figures) are<br />

given in this report. The costing information is published in a separate document.

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