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Intercollegiate Rocketry Engineering Competition (view source)
Revision as of 07:46, 8 July 2018
, 07:46, 8 July 2018Created page with "The '''Intercollegiate Rocketry Engineering Competition (IREC)''' is hosted annually in June by the Experimental Sounding Rocket Association (ESRA) at Spaceport America in New..."
The '''Intercollegiate Rocketry Engineering Competition (IREC)''' is hosted annually in June by the Experimental Sounding Rocket Association (ESRA) at Spaceport America in New Mexico. The competition requirements are to build a rocket with solid, hybrid, or liquid propulsion capable of delivering an 8.8 pound payload to either 10,000 or 30,000 feet. The most recent team, [[IREC 2018]], was the second SSI team to participate in the competition, and won second place in the 30k commercial off-the-shelf motor category.
= Overview =
The competition is split into six different categories across the two altitude targets and three motor types: commercial off-the-shelf solid motors (COTS), student researched and developed solid motors (SRAD), and student researched and developed hybrid or liquid motors (hybrid/liquid). Teams are judged on their performance in a number of categories:
* Poster and podium presentations at a conference day
* Technical report on the project
* Quality and construction of the rocket
* Quantity of student researched and developed components
* Flight performance and closeness to the altitude target
* Payload design and originality
= Overview =
The competition is split into six different categories across the two altitude targets and three motor types: commercial off-the-shelf solid motors (COTS), student researched and developed solid motors (SRAD), and student researched and developed hybrid or liquid motors (hybrid/liquid). Teams are judged on their performance in a number of categories:
* Poster and podium presentations at a conference day
* Technical report on the project
* Quality and construction of the rocket
* Quantity of student researched and developed components
* Flight performance and closeness to the altitude target
* Payload design and originality