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ESA Document - Emits - ESA

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s<br />

HMM<br />

Assessment Study<br />

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

February 2004<br />

page 98 of 422<br />

• EVA-supported completion of MEV structural I/F<br />

• MEV Check-out, Commissioning Phase & Crew orientation commence at<br />

MEV delivery<br />

Once the MEV is added to the composite, the 90-day commissioning phase begins. If an in-orbit<br />

crew is required, dedicated commissioning crew shall be present for the first 60 days.<br />

Service Platform 5<br />

2.8.3.9 Launches 26-27- Crew<br />

Figure 2-56: Launch of MEV<br />

EVA<br />

Airlock 1<br />

Habitation Module<br />

• Launch 26 & 27 - Mars Crew delivery 30 days before departure<br />

– assumption, two launches of three crewmembers by Soyuz<br />

– alternative, single launch by shuttle<br />

2.8.3.10 Launch 28- Cryogenic stage refueling (if required)<br />

• Refueling of Cryogenic stages performed during commissioning phase<br />

Note that the above assembly approach satisfies the constraint to minimise the Cryogenic fuel<br />

boil-off. However the assembly of the habitation modules at the beginning of the composite<br />

assembly sequence maximizes the life requirement of the equipment.<br />

Table 2-34 show a summary of the sequence defined above:<br />

MEV

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