Static Test Fires
Ensures the engine’s optimal performance and reliability
Static Test Fire #1
November 23rd, 2019
On November 23rd, 2019, the UCI Rocket Project conducted its first-ever static test fire of our Preliminary Test Engine (PTE). Static test fires, in the horizontal configuration, are used for engine development. During the test fire, we achieved 3 seconds of burn time with a maximum thrust of 740 pounds. A promising start for the rocket!
Static Test Fire #2
November 21st, 2020
Almost a year after our first test fire, we once again tested our Preliminary Test Engine (PTE). In addition to verifying the characteristics of the engine, this test fire also proved the functionality and efficiency of the Cold Brew mobile test stand. Unfortunately, this test was unsuccessful. The Liquid Oxygen fuel did not flow during the engine fire, leading to only the Liquid Nitrogen burning. This created an impressive plume of fire, but no thrust was created.
Static Test Fire #3
April 17th, 2021
Coming off an unsuccessful test fire a few months prior, we completed our third test fire of the PTE in April 2021. A testament to the team’s hard work, this test fire gave incredible results. According to our data, the engine burned for 7 seconds and produced 950 pounds of thrust, with 880 pounds being produced at steady state. An incredible improvement from the first test fire, the future of our engine was promising. As a result, we began preparation for VTF: testing the rocket in launch configuration.