with the help from Colin Sledge , we successfully tested the parafoil for the precision landing system. The decent rate is good for testing the precision landing system.
UCI Rocket Project: Mold for hybrid engine nozzle diverging part has been printed.
This is the mold of diverging part of the hybrid engine nozzle. it took 33 hours to print.
UCI Rocket Project: We have finished the fabrication of active gimbal !
We have finished the fabrication of vector thrust gimbal system This is the test video : https://www.youtube.com/watch?v=fT_OfHLh5ao
Rocket Project Liquid Engine Final Design
We have finalized the design for our liquid engine. We have finished the manufacturing of Nozzle and Combustion Chamber. If we have enough funding, we will manufacture the injector plate.
Rocket Project Hybrid Engine Thermal Analysis
We have developed a MATLAB code to do the hybrid engine thermal analysis.
Rocket Project Rockoon Platform Avionics System Ready for Test
We have finished the coding of avionics system. We are currently doing the reliability test. We will test this avionics by using high altitude balloon on spring break
Rocket Project gimbaled Thrust active stabilization system updates
We have finished the CAD design and 3D printed the prototype. We will finish the assembly by end of this week.
Rocket Project Rockoon Platform Updates
We have successfully laser cut the Kevlar rings for the gimbal system and the square plate.
Rocket Project Hybrid Engine Test Stand Done.
We have finished our test stand for the hybrid engine static fire test.
UCI Rocket Project (UCIRP) Finalized Design of Prototype 2 Rockoon System
Fabrication of the Prototype 2 Rockoon System will begin this week. The Prototype 2 is designed to elevate a 1 meter long rocket to an altitude of 20 km. Once this target altitude is reached, the Prototype 2 Rocket will be launched autonomously and both the Rocket and Rockoon System will return safely to the ground. Launching a sounding rocket …
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