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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 315 of 422<br />

The used frequencies (in Table 4-21) and data rate will be taken from the protocol. The<br />

maximum data rate allowed, 2048 kbps, will be used. Figure 4-61 shows the frequency plan and<br />

data rate for EVAs.<br />

Due to the wavelength of the UHF signal (around 1.75 m), the effect of Martian dust on the<br />

signal propagation is negligible.<br />

The communications system in the space suit is similar to the one used in ISS. The radio has two<br />

single UHF channel transmitters, three single channel receivers and a switching mechanism. The<br />

low profile antenna is located in the (Portable Life Support System) PLSS.<br />

Forward link (EVA->Base) Return link (Base->EVA)<br />

Frequency See Table 4-21.<br />

Data link layer protocol Proximity link<br />

Data rate 2048 kbps 256 kbps<br />

Coding Convolutional, rate ½, constraint length 7 Viterbi code.<br />

Modulation scheme Bi-Phase-L modulated directly into the carrier<br />

Modulation index 60º +/- 5%<br />

Bit Error rate 10 -11 , obtained Eb/N0 = 8.4 dB<br />

Doppler and Doppler rate Negligible<br />

Table 4-20: Characteristics of the UHF link<br />

UHF Forward Return<br />

channel (MHz) (MHz)<br />

1 435.6 404.4<br />

2 437.1 401.6<br />

3 439.2 397.5<br />

4 444.6 393.9<br />

5 449 390<br />

Table 4-21: UHF proximity link protocol channels.<br />

Figure 4-61: EVAs data rates and frequencies, respectively

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