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ESA Document - Emits - ESA

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s<br />

Body-mounted radiator<br />

facing sky<br />

Lateral body mounted<br />

radiator<br />

Bottom body mounted<br />

radiator<br />

Advantage Disadvantage<br />

Low sink temperatures (max is -120C) and<br />

good stability (20K variation max over one<br />

sol) => high performance radiator when not<br />

illuminated<br />

Possible combination with the ascent vehicle<br />

radiator necessary during RdV<br />

Partial viewing to the sky increases the<br />

radiator performance when not illuminated<br />

Adequate to a close location with the confined<br />

compartment (secondary loop system) if<br />

chosen on the lower part of the SHM<br />

Permanently shadowed by the SHM body =><br />

the amplitude of the sink remains low and the<br />

sink close to the night temperatures (high<br />

sensitivity to sun illumination)<br />

Adequate to a close location with the confined<br />

compartment (secondary loop system)<br />

The radiator view factor is closed when<br />

docked to the transfer vehicle (low activity of<br />

the SHM during transfer, the heating budget is<br />

therefore minimised)<br />

Deployable radiator Possibility to implement a tracking of the Sun<br />

to minimise illumination of the radiator<br />

Table 4-11: Radiator options<br />

HMM<br />

Assessment Study<br />

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

February 2004<br />

page 284 of 422<br />

Only location is on top of the ascent vehicle<br />

already occupied by the solar cells necessary<br />

during rendezvous.<br />

Radiator Sun illumination is maximal over one<br />

day<br />

Possible dust deposits<br />

Sink temperature depends on the viewing with<br />

sky and ground => instability of the sink<br />

(large amplitude of the ground sink)<br />

Possible illumination during a few hours<br />

Viewing of the sky degrades when too close to<br />

the ground<br />

The dust density is higher close to the ground<br />

(possible electrostatic adhesion)<br />

Conflicts with the heating from braking<br />

thrusters => requires specific protection<br />

Gravity and wind pressure penalize mass<br />

4.3.4.3.1.3 Radiator sizing<br />

Figures here below indicate the relative penalty of the radiative surface to the daily variation of<br />

the environment, this if the cooling capability is to be maintained.<br />

In the case of a bottom radiator, how much the ground can heat up with convection and the SHM<br />

rejection will depend on the nature of the ground. The rather low thermal inertia in general does<br />

not make this option attractive, in particular when considering that the ground has little means to<br />

cool down itself if the two surfaces are parallel (so the ground will tend to the mean daily<br />

radiator temperature).<br />

In the case of a lateral cylindrical radiator, assuming a view factor of 0.5 to sky and ground,<br />

equinox, latitude 0, at noon the penalty is a ratio of 2.4 against the same heat rejection at<br />

–120C (end of night). The negative impact of the Sun remains acceptable when considering its<br />

angle of incidence (left figure). Increasing the view factor to the sky increases the rejection but<br />

also increases the Sun illumination (intensity and duration), however at a much lower rate.

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