April 2015
Intermediate to advanced
480 pages
21h 24m
English
Let’s start with the Apollo example from Chapter 14. Recall that in Chapter 14 we defined nine decisions and a number of allowed values for each decision (such as EOR yes or no, command module crew of 2 or 3, service module fuel cryogenic or storable). We also had a way of measuring how good an Apollo architecture is by means of two metrics: total launched mass (IMLEO) and probability of mission success. We used the rocket equation to link mass to the decisions, and a risk table gave us the probability of mission success for each combination of decision variables.
This example can be formulated in such a way that we have a set of architectural decisions
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