University of Hawaii Community Colleges


 

Mission Statement:

To conduct research on the feasibility of using a sublimation–fueled motor for providing low-power venier thrust. The specific impulse of the sublimate camphor will be determined by a static ground test and by deploying the rocket from a sounding rocket at apogee. On board cameras will record the sublimation rocket’s flight parameters. This data will be supplemented by an IMU and a multi-axis accelerometer that will provide a baseline for the payload’s flight trajectory. In addition, a proof of concept test will be performed on a 1U Artemis CubeSat.

 

UHCC RSX 2022 TeamPic 1

UHCC RSX 2022 TeamPic 2 

 

Deliverables 

Design Reviews
CoDR   PDR   CDR
         
Integration and Test Reviews
STR ISTR FMSR VVCC -
         
Interface Documents
TM ICD PWR ICD Pins PWR Budget Timer Events

Mech. Drawings

  Electrical Schematics
         
Check Out Procedures
  May 2021   June 2021   
      Video    
Final Report
     PDF