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Functional architecture
Top level Vehicle
Requirements Breakdown Structure
ConOps Nominal StagesRequirement statements, Generated by project stakeholders (This still needs to take place):
1.0. Vehicle should fly to an altitude of 30 000 ft.
2.0. Vehicle should stay in constant communication [of telemetry] w/ ground through ConOPS stages 2-10.
3.0
ConOPS Stages
These are the distinct states of rocket
1.0 Assembly - 2.0 Ground functions - 3.0 Launch - 4.0 Powered Flight - 5.0 Coast - 6.0 Apogee Events - 7.0 High velocity Descent - 8.0 Low altitude Events - 9.0 Low velocity Descent - 10.0 Landing - 11.0 Recovery & Disassembly
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