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.
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 |
Electrical Schematics | ||||
Check Out Procedures | ||||
May 2021 | June 2021 | |||
Video | ||||
Final Report | ||||