Stevens Institute of Technology


 

SIT TeamPhoto2 

Mission Statement:

1) To create a system to record and reduce vibrations occurring in a payload during launch for sensitive electronics and other equipment.
2) To measure High-Speed Boundary Layer Transitions from laminar to turbulent pressure waves using a high and low frequency pressure sensor combination mounted in a custom window on the skin of the rocket.

Deliverables:

Design Reviews
CoDR   PDR    CDR
Integration and Test Reviews
STR ISTR   FMSR LRR
Deliverables

Mech. Drawings

Power Budget Electrical Schematics
Check In Procedures
  Preliminary   Final  
Final Report
     PDF    
Project Poster
     PDF    
         

 

 

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