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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 112 of 422<br />

It is not excluded that special components/instruments are controlled within boundaries set by<br />

the major tasks via special centres (called National Control Centres in Figure 2-60).<br />

2.10.2.2 Major mission tasks<br />

2.10.2.2.1 Launches<br />

Ariane<br />

It is assumed that the Ariane launches are based on a derivative of the ATV launches. The<br />

operation of the ATV is assumed to be performed by the CNES ATV operations centre. The<br />

approach and associated recurrent costs are assumed to be similar to currently planned ATV<br />

operations at the ISS.<br />

Because of the complexity of the cargo and its sophisticated subsystems a purely passive launch<br />

is not assumed, so the cargo operations therefore require an operational effort. This is assumed to<br />

be provided by the LEO Assembly task.<br />

Considerable nonrecurrent effort is required to develop the launch, rendezvous and docking<br />

concept under consideration of the safety and complexity of the to-be-assembled large<br />

composite. This effort is shared between the Ariane launch task and the LEO Assembly task.<br />

Proton<br />

It is assumed that the Proton launches are based on a derivative of a Russian upper stage (e.g.<br />

Fregat-based TBC). The operation of the vehicle is assumed to be performed in Russia. The<br />

approach and associated recurrent costs for the upper stage operation are assumed to be similar<br />

to currently planned Soyuz flights to the ISS. The effort is assumed to be included in the launch<br />

costs.<br />

Because of the complexity of the cargo and its sophisticated subsystems a purely passive launch<br />

is not assumed TBC, the cargo operations thus require a TBD operational effort. This is assumed<br />

to be provided by the LEO Assembly task.<br />

Considerable nonrecurrent effort is required to develop the launch, rendezvous and docking<br />

concept under consideration of the safety and complexity of the to-be-assembled large<br />

composite. This effort is shared between the Proton launch task and the LEO Assembly task.<br />

Soyuz<br />

The Soyuz missions are assumed to resemble those to the ISS. The missions are bought in<br />

Russia.<br />

Energia<br />

For the delivery of the composite elements to the assembly composite it is assumed that the<br />

Energia’s upper stage is used. This may introduce some design changes in the actual design of<br />

the RCS.<br />

As far as the Energia launch to low circular orbit is concerned, this is bought including<br />

operations in Russia.<br />

The upper stage operations are assumed to be directed from a dedicated operations centre.

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