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Vehicle | Mass | Length | Motor Selection | Recovery | Primary Materials |
|---|---|---|---|---|---|
| Therion | 70lbs | 12ft 2in | M3400 | SSDD | Carbon Fiber, Fiberglass, Aluminum |
Full Render:
Critical Design Review:
MIT Rocket Team CDR Presentation Slides.pdf
Executive_Summary_IREC2016_CDR.pptx
Flight History:
| Vehicle | Motor | Launch Site | Date | Result |
|---|---|---|---|---|
| Therion I | M3400 | MMMSC | GSE Failure; Loss of Vehicle | |
| Therion II | M3400 | MDRA | Reefed Drogue, No Main | |
| Therion III | M3400 | IREC | Main Failed to Deploy |
Therion-III-Post-Flight-Analysis (1).docx
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