Created
June 5, 2018 13:22
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A sample of extracted requirements for use with ModelCI. Derived from the SysML Spacecraft Definition by Sanford Friedenthal and Christopher Oster https://github.com/actiontofu/architecting-spacecraft
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| /ModelCI/TestCase|3.1.1|Mass|<|2000 | |
| /ModelCI/TestCase|3.1.2|Thermal Protection|=|1 | |
| /ModelCI/TestCase|3.1.3|Electrical Power|=|1 | |
| /ModelCI/TestCase|3.1.4|Payload Accomodation|=|1 | |
| /ModelCI/TestCase|3.1.5|Orbit Constraints|=|1 | |
| /ModelCI/TestCase|3.1.6|Structural Integrity|=|1 |
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