Evaluating and purchasing a communications satellite system - Satellite and Launch Vehicle Costs

From INVESaTWIKI

Satellite and launch vehicle costs

The costs for the satellite and launch vehicle are major and up-front. The satellite should be compatible with a variety of launch vehicles. Particularly because the worldwide launch providers are combining their capabilities across continents for total mission assurance and on-time schedules. Examples are Proton (Russian) backing up Atlas (USA), and Arianespace (French) securing back up from Sea Launch (USA/ Russian) and Mitsubishi Heavy Industries (Japanese). Operators may choose a ‘delivery in orbit’ proposal, or purchase the satellite and negotiate their own launch and insurance package. Either way, the satellite specifications, mass and dimensions have a significant impact on the choice, price and insurability of the selected launch vehicle. Total mission assurance by the launch providers has been shown to have a beneficial effect on the insurance industry.
The initial purchase price is the largest factor (70 to 80 percent) in the TCO a business buyer faces in selecting a satellite platform.
What is not always obvious is the relationship between the initial costs of the satellite relative to its projected lifetime cost. For example, building in superior margins for critical subsystems may result in higher upfront costs, but can result in a significantly lower TCO. Other factors such as insurance, customer support and lifetime reliability also affect the total system cost.
Major in-orbit anomalies are unpredictable, but by researching all satellite models, operators can identify those with records for the fewest and least expensive anomalies.
Bus anomalies have occurred in the satellites of all manufacturers. They have been attributed to faulty design and most frequently to faulty manufacturing of components. At the time of the evaluation of the design, the manufacturer’s current performance on the satellite he is offering should be key in the evaluation. Operators should evaluate the anticipated system costs from an overall performance perspective, balancing subsystem power margins against the expected life of the satellite. For instance, if a solar array design starts life with a power margin of 25 to 20 percent, it is less likely to have problems fulfilling lifetime performance if the spacecraft is built with a power margin of 25 to 30 percent. The same concept applies to many subsystems, such as batteries, radiation resistance, etc. The additional power margin may cost more up front, but can add years to the life of the spacecraft and generate additional revenues over mission life. [1]



References

[1] Satmagazine.com - January 2004
Satellite System Acquisition: A Fresh Approach to Evaluating and Purchasing a Communications Satellite System

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This page has been accessed 310 times. This page was last modified 15:54, 17 October 2006.


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