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[[File:Launch1PrepOlympus2019.JPG|400px|thumb|right|frame|The team setting up the rocket on a pad at FAR for the first test launch of the year.]]
 
[[File:Launch1PrepOlympus2019.JPG|400px|thumb|right|frame|The team setting up the rocket on a pad at FAR for the first test launch of the year.]]
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Olympus 2019 was the third SSI team to compete in the [[Intercollegiate Rocketry Engineering Competition]], succeeding [[IREC 2018]]. The rocket featured a compact avionics bay, a redesigned recovery system, a fiberglass airframe with a carbon fiber fin lay-up, and a protein crystallography payload. A liquid propulsion system was designed and tested as over the course of the year, although it was ultimately not flown in New Mexico. This liquid motor was a continuation of the prior year's Helios project, and used many of the same design principles, and Olympus 2020 is hoping to fly the liquid motor at IREC next year.
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Olympus 2019 was the third SSI team to compete in the [[Intercollegiate Rocketry Engineering Competition]], succeeding [[IREC 2018]]. The rocket featured a compact avionics bay, a redesigned recovery system, a fiberglass airframe with a carbon fiber fin lay-up, and a protein crystallography payload. A liquid propulsion system was designed and tested as over the course of the year, although it was ultimately not flown in New Mexico. This liquid motor was a continuation of the prior year's Helios project, and used many of the same design principles, and [[Olympus 2020]] is hoping to fly the liquid motor at IREC next year.
    
=Overview=
 
=Overview=
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