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ESA Document - Emits - ESA

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s<br />

Two system options were presented with following mass budgets:<br />

ECLSS power requirements<br />

The results are shown in Table 4-69.<br />

Today’s Technology<br />

Mass consumables (kg) 46<br />

Mass system (kg) 549<br />

Table 4-68: Mass budgets<br />

Characteristic Value<br />

Power requirement day (W) 375<br />

Power requirement night (W) 375<br />

Table 4-69: Power budgets<br />

HMM<br />

Assessment Study<br />

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

February 2004<br />

page 398 of 422<br />

ECLSS volume requirements<br />

Only a first estimate for the volume of the life support system has been achieved in the course of<br />

the study. The internal volume requirement pertains to the volume occupied by the ECLSS inside<br />

the pressurised vessel, as opposed to the external volume requirement, which pertains to the<br />

volume needs outside the pressurised volume.<br />

4.5.9 Data handling<br />

See 4.3.6.<br />

4.5.10 Communications<br />

4.5.10.1 Requirements and design drivers<br />

Characteristic Value<br />

Internal volume requirements (m3) 1.4<br />

External volume requirements (m3) 0<br />

Table 4-70: Volume requirements<br />

• The vehicle shall support Tracking, Telemetry and Command (TT&C) communications<br />

during all mission phases and any attitude.<br />

• Communications availability should be maximized.<br />

• The telecommand (TC) and telemetry (TM) data rates shall be selectable to improve the data<br />

rate depending on the distance to the receiving unit.<br />

• Data consists of housekeeping, audio, and any additional data.<br />

4.5.10.2 Baseline<br />

4.5.10.2.1 Links

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