History

A year-by-year look into our past


Our team has come a long way over the years since we were first formed in 2010. This timeline is meant to preserve the milestones and accomplishments, as well as our failures that we have had at a team. There are some parts of our past that are not well known, if you have further details, pictures, or information about our team from years ago, please send us an email at rkt-team@umn.edu and we would love to chat about your experiences with/on the team.

2022-2023

The 2022-2023 school year brought with it the return of multiple large scale projects, but also yet another year of amazing success at the 2023 Spaceport America Cup. The team had one of their most successful years thus far at Spaceport, bringing home two awards, as well as being the overall highest point earner across the entire competition! Meanwhile, the team heavily was focused on development of our largest rocket as part of our High Altitude Project attempted Spaceshot rocket. It was by far the busiest year the team has had, with countless new projects, rockets, and ideas being worked on tirelessly throughout the year. 

Spaceport America Cup - Returning Champions 

This year, with the High Altitude project being the primary focus on the team, the SAC project was not as heavily invested in as seen in previous years.  However, that did not stop the team from returning to the 30,000 ft SRAD category, with a rocket named Crimson Stratus. Crimson Stratus was flown on our previously validated motor developed in 2020 named Charlie, a 94% O-class motor. 

Despite this being a secondary project this year, the team still continued to find a few more innovative systems to include on the vehicle, including a custom student design and machined 5-port pitot-static tube, an upgraded recovery harness, and more optimized composite body tubes and fins. The standard on the team at this point has been near-100% SRAD designs and systems across the entire vehicle, which has been continued into the design of Crimson Stratus this year.

As part of the competition, the team was also selected to present a podium presentation on the Pitot-Static tube, highlighting the testing that was done at Collins Aerospace Transonic Wind Tunnel, and the machine learning data analysis from calibration. 

Due to high winds at the competition, Crimson Stratus was not able to be launched until the second day of flying. However it was well worth the wait, as the flight was more perfect than the team could have hoped for, with a perfectly straight boost, flawless recovery deployment, and a relatively easy recovery. The only damage seen was minor scratching along the length of the vehicle, as it was dragged over 150 ft after landing due to the still relatively high winds. To make things even better, the team discovered upon recovery that the rocket flew to just 53 ft off of the simulated altitude for the flight, with an expected altitude of 29,500 ft and an actual achieved apogee of 29,447 ft -- a difference of just 0.18%! 

With an exceptional performance, the team won two awards, first place in the 30,000 ft SRAD Solid category, as well as first place for the James Barrowman Award for Flight Dynamics because of the 0.18% altitude difference! Alongside that, the team was also named a finalist for the Charles Holt award for Modeling and Simulation, but even more impressive was the the team was the HIGHEST SCORING team across the ENTIRE competition! 

High Altitude Project - Spaceshot Attempt

Easily the most ambitious project by far our team has attempted, the High Altitude project focused on a rocket named Phoenix this year. Ultimately the flight was not successful in the end, but so many impressive challenges were solved along the way on this project. 

The launch occurred in the Black Rock Desert in Nevada, specially arranged in part with Tripoli Minnesota to host a Tripoli "Minnesota" launch in the deserts of Nevada. With this opportunity available, the team set their goals high, initially trying to pass the Kármán line (100 km, or 328,000 ft). As the project developed throughout the year, and to ensure that the vehicle stayed within the Tripoli Safety Code, the goal was shifted slightly to target a lower altitude, closer to 300,000 ft. The reason for this shift was that the team was prioritizing having a safe flight of the vehicle, rather than trying to cut safety margins too thin in an effort to reach the 328,000 ft Kármán line. 

The launch was originally scheduled to occur in May 2023, but was pushed back to the end of July 2023 due to wet conditions at the Black Rock Desert playa, as well as to allow more time to make and process the impressive 240 lbs of propellant that would be used to boost Phoenix near the edge of space. Phoenix was an 8" sub-minimum diameter rocket standing 18.5 ft tall, with a loaded weight of 485 lbs. The motor, named Helena, made up an impressive nearly 400 lbs of that weight, and stood over 10 ft tall.  Helena was an R-class motor, with an average thrust of over 23,000 N, and a burn time of 10.4 seconds.

On July 29th, 2023 at 2:16 PM, Phoenix lifted off and had a beautiful first two second of the motor burn, but at 2.4 seconds into flight at ~2,000 ft AGL, the motor CATO'd, quickly ending the flight and sending the rest of the vehicle to plummet to the ground. Failure analysis indicates the motor experienced an overpressurization due likely to two main factors, first that there were some locations within the propellant with excessive voiding, as well as the peak pressure and thrust, which was expected to occur right around the time of the explosion, was much higher than simulated. All individuals were standing at a safe standoff distance, and no people or property was damaged in the failure. Although it was a very disappointing end to a significant effort on behalf of so many team members, it was an impressive but brief flight, and an impressive CATO to see firsthand. 

GOPHER Project Expands to Certifications

In an effort to improve the individual learning of each new recruit on our team, in Fall 2022 GOPHER orientation project shifted gears to have each new member design, build, and launch their rocket, one that they would be able to become Tripoli Level 1 certified with! Under the new program, one mentor would meet with groups of 4 to 6 students to help guide them through the design and build of their first rockets. A shockingly high number of new students were wanting to build their own rocket, with over 80 students finishing their rocket, and in just one day 61 members attempted their certification flight-- with 53 members successfully getting certified! It was a windy day for flying, but otherwise a beautiful day to get a whole new group interested in rocketry. The following weekend, 5 more students were able to get their certifications through the program as well!

Special Projects Advances Testing & Building

Special projects focused their efforts on a few key tasks to support the large demands for ground support and testing, primarily from the High Altitude project. This included the development of Gold Celedon, a 4" diameter test rocket capable of flying between 1,000 ft and ~8,000 ft, with the main purpose being to test different recovery systems. Gold Celadon became the most flown rocket in team history, achieving 7 flights by the end of the school year, with plans to continue use in the future.

Additionally, the team spent a significant amount of time and effort converting the team's launch tower from a rail configuration into a tower configuration for the High Altitude spaceshot flight. After a year of careful modifications, the tower performed perfectly to lift the High Altitude Project, Phoenix, off the ground. 

2021-2022

The main focus of the year was spent on development of our rocket Iridium Sandstorm for Spaceport America Cup (SAC). The largest rocket the team has built so far was created, standing 15.5' tall, having an OD of 8.5", and weighing a massive 260 lbs fully loaded. It was also the team's first go at an 8" SRAD motor, which also included our first attempt at finocyl grain geometry. The motor performed beautifully in static fires and in flight, and was unofficially named Jennay. Other highlights included a near fully SRAD design (including airframe, parachutes, motors, and most flight computers), the second flight of the Universal Flight Computer (UFC), and an active control module designed by an AEM Senior Design team featuring a reaction wheel for roll control and air brakes for apogee control. 

Due to the large size of the rocket and being unable to go beyond an O-class motor due to competition regulations, the team decided to move down to the 10k SRAD category. The competition flight was less than ideal, as a premature separation caused the rocket to only reach 4100 feet due to drag separation from excessive air brake deployment combined with miscommunication on expected drag forces the air brakes would be creating. Overall, the rocket survived its plummet from the sky, suffering only from some shredded parachutes. 

Meanwhile, in other areas of the team, the High Altitude project took a step back due to issues finding a suitable launch site combined with the difficulties of balancing two large and time intensive projects on the team. The team moved away from the Midwest rocketry competition as we were beginning to outgrow it, and the Special Projects team was formed in its place which was able to launch a recovery test rocket 6 times throughout the year as well as constructed a massive 24 foot tall launch tower that was used at Spaceport America cup. 

2020-2021

2021 was a year of success like no other for the team. In June of 2021, our team took home the first place award in our category at SAC (30k SRAD) AND were also chosen as the overall competition winners out of 76 teams! Additionally, the team took our first journey to Friends of Amateur Rocketry (FAR) launch site in the Mojave Desert to attempt our highest altitude launch yet. 

Spaceport America Cup - Champions

The COVID pandemic was still lingering, which caused the competition to be held virtually, but that did not stop us from building and launching our competition rocket named Thunderyeet.  

Thunderyeet was launched at the local Tripoli Minnesota launch site in North Branch, MN in June 2021, flying on our SRAD 6" diameter motor named Charlie. The motor was flown with one grain removed to a lower altitude of 19,000', as the standing waiver was only 20,000'. The rocket design was similar in many aspects to previous competition years, but new was our first iteration of our fully student designed and developed Universal Flight Computer (UFC), meant to be a modular system that was easily adaptable from year to year. The flight was mostly successful, except for the parachutes shredding due to suspected high horizontal velocity at deployment. Despite this, the rocket remained nearly completely unharmed minus some chipped paint.  

The year was challenging in many new ways, due to COVID there was strictly no access to our team's lab space in the fall semester, and in the spring only four people were allowed in the lab at a time to comply with social distancing guidelines, causing our rockets were built on a more last-minute compressed timeline. Recruitment for the team was at an all time low due to the pandemic as well. Fun fact: of our 17 different leadership positions on the team, not a single one was contested during the spring elections! 

High Altitude Project

The High Altitude team reached for their highest altitude yet: 100,000 feet. This rocket was known by many names, with an official name of Kuiper, but was commonly referred to instead as Hot Rod, or even just "Kevin", which was the name of the motor used. This sub-minimum diameter rocket was 4" in diameter and just under 13 feet tall, and to some looked more like a pole than a rocket due to the disproportionately small fins on the rocket (which were designed this way to help maintain a stable flight throughout the entire flight profile). The ~O6,000 motor with around 23,000 Ns total impulse occupied the majority of the rocket. There were many firsts in this rocket for the team, including the first time making two new parachute types (annular main, disc-gap-band drogue), using cable cutters for main parachute deployment, having a welded steel fincan, and first time launching at the FAR site in California.

This rocket took three lower altitude test flights of various components to gain enough confidence in the systems to launch out at FAR. Despite all the preparations, on Sept. 4th, 2021 when Hot Rod took to the skies, there was a structural failure of the aluminum body tube at around 3,500' AGL which caused the top half of the rocket to break off, and Kevin went soaring off into the skies without the rest of the rocket to lead the way. The failure occurred due to a combination of thin body tubes, a weld joint, and high bending moments. Kevin was later recovered by the launch site staff a few months later, and as of Spring of 2023, the team has finally been reuinited with our beloved motor after paying a hefty shipping fee. 

2019-2020

The COVID Pandemic caused a University wide shutdown along with nearly every competition being cancelled. This year was primarily a hiatus for the team as we were unable to work on anything in person beginning in March. Some additional online research took place during the last few months of the school year, but ultimately there was no resources or ability to complete any of the projects started earlier in the year. 

The one exception to this was the Alka Challenge held in Dec. 2019, which our team held on to our title, again claiming the 1st place prize and $25,000 for the team. This has been the final year of the competition as it was halted due to the pandemic. 

2018-2019

Spaceport America Cup

Moving into 2019, our team had the first taste of victory at Spaceport America. We again continued to compete in the 30k SRAD category and took home first place with our rocket named "Thunderstroick VII: The Stroick Awakens". This 6" minimum diameter rocket was powered by our motor named "Sheila", which had a beautiful flight besides some minor recovery problems (parachutes tearing) on the way down which resulted in a bent fin on landing. 

High Altitude Project

Our High Altitude team also launched the same week at Spaceport America as an exhibition launch, using a Cesaroni N2540G to launch a 4" sub-minimum diameter rocket to 44,910 ft, setting the highest altitude recorded for the team. As of 2022, this altitude still remains the highest the team has successfully flown to, despite later attempting higher altitudes.  

Alka Rocket Challenge

Near the end of 2018, our Alka Rocket team returned to Bayer's campus in Florida to make another attempt at the world record of highest rocket powered by Alka Seltzer tablets. Our team was again victorious in the unconventional rocketry competition, taking home the 1st place trophy along with $30,000 to help fund our team. 

Further details of this rocket and competition can be found on our Alka page. 

2017-2018

Countless opportunities for new projects continued to present themselves, as again the team picked up another project that was a bit unconventional for rocketry called the Alka Rocket Challenge. The team took a year off of launching for the high altitude project, but still continued work in other projects including Spaceport America Cup, Midwest Rocketry Competition, and our own GOPHER project.

Alka Rocket Challenge

The company Beyer released a new competition to occur in the fall of 2017, with the idea of using the pressure generated from gases released by Alka Seltzer tablets to be used to power a rocket. They challenged college teams to see who could beat the world record, and lured in teams, including ours, with the grand prize of a $25,000 check to the winning team. 

These rockets were much smaller in scale than we were used to (think model rocket size), and of course was a bit unconventional mode of propulsion. Despite that, a group on the team formed ready to take on the challenge. In December of 2017, we were proudly named the Guiness World Record holders for highest Alka Seltzer powered rocket, reaching 429 ft AGL. 

Spaceport America Cup

The team took on the 2018 SAC challenge in hopes from some redemption from the previous structural failure from the year before. The rocket was named "Thunderstroick IV: A New Hope" (a mashup between Star Wars and our mentor Gary Stroick's last name) and we were again competing in the 30k SRAD category. 

Unfortunately, as the rocket approached mach 1 a structural failure occured as the fins failed due to flutter. This was due to the fiberglass fins simply being too thin. This ultimately led the team away from composite fins for a while, in future years opting for a welded aluminum fincan instead. 

2016-2017

2015 was the team's first jump into multiple projects, and of course we couldn't stop with just two, so in 2016 the High Altitude team was formed as well as the GOPHER team, which was our introduction/orientation to rocketry for newer team members. The second year of our participation in the Midwest rocketry competition was successful as well, with our team taking home the 2nd place trophy. 

Spaceport America Cup

2017 marked the first year that the competition had shifted over to the new launch site at Spaceport America in New Mexico, and was then renamed Spaceport America Cup. Our team competed in the 30k SRAD category under a rocket named "Maroon Flyve", moving back to what would become our standard 6" minimum diameter rocket design for the next few years. 

This year the team continued to do some great development on our solid rocket motor development, and the team's first static fire on an O-class motor successfully occured. This flight was the return of our SRAD motors to competition, which was done on an ~O4600 (37,000 Ns) motor. Other highlights of this rocket include use of both fiberglass and carbon fiber airframes, further development on the rover payload, continuation of pitot tube and SRAD flight computers, controlled canards, and parachute reefing. Unfortunately there was a structural failure of the rocket and the tubes were zippered during flight.  

High Altitude Project

This was the year of the beginning of the rise of  the High Altitude project, despite remaining a relatively small portion of the team. The high altitude team was not intending to compete in any regular competition, instead as we like to call it it's a competition with the sky, where we were truely just trying to see how high we could launch on solid rocket motors. 

This project launched as an exhibition launch at Spaceport America in 2017, flying a 54mm minimum diameter rocket to an attempted 40k feet. The motor had a failure where the nozzle blew out on ascent which reduced the apogee from 40k ft to 20k ft. This rocket was originally intended to be an upper stage for a two stage rocket in the future that would be capable of going to over 100,000 ft, however the team is yet to have made a two stage rocket.

GOPHER Project

With an ever-expanding team, it became clear that there was a need to better educate new team members on the basics of rocketry. GOPHER was introduced as a way for experienced/senior members of team team to mentor smaller groups of students through building a small L1-style rocket. Why was it named GOPHER? It is an acronym standing for the Grand Opening Project to Help Educate Rocketeers, and is also our school's mascot! 

2015-2016

Our team continued to grow fast over the past few years, at this point exceeding 70 members. This was the final year that the Intercollegiate Rocket Engineering Competition (IREC) was hosted in Utah. The goal of the year was to launch to 20,000' in the "Advanced Category" at IREC on our SRAD propulsion system, however due to issues finding a suitable location to produce our solid rocket motors, the team dropped down into the "Basic Category" to be able to continue competiting at this year's competition. 

We went with a larger 7.5" diameter rocket to help accomidate our semi-autonomous Rover payload that had been in the works over the past few years. New construction techniques were used throughout the rocket, including making the airframe out of a mix of Kevlar and fiberglass. The avionics team also made a number of advancements, expanding and improving on their work with the pitot-static system, custom flight computers, and ground station. The recovery team took their first shot at parachute reefing, with a goal of trying to save space and have just one parachute in the rocket. Due to the last minute switch in propulsion systems caused by restrictions that were out of the team's control, this rocket ended up flying on a Cesaroni N250W motor. Additionally, a new subteam was formed this year dedicated to Simulations, working on learning more about fluid theory, structural mechanics, and their implementation into ANSYS. 

During flight there was a failure of the deployment system, causing it to crash into the desert floor at very high speeds. This left the bottom ~2 feet of the rocket somewhat intact, a ~1 foot section of crumple zone, and fragments of the remainder of the rocket across the desert floor. Despite the unideal performance of the rocket, the team had great success at the competition taking home the first place title for the Payload Challenge, with our small two-wheeled rover, as well as the first place Team Spirit award! 

This year also marked our first year competiting in the Midwest Rocketry Competition, a local competition that is held annually in May in North Branch, MN by the Minnesota Space Grant Consortium.  Our Midwest archive page steps through the competition challenge throughout the years including the rockets we have built for each of these challenges. 

2014-2015

In 2015 the team competed in IREC's "Basic Category", wow-ing the competition with the tallest rocket in our category. The rocket soared to an apogee of ~8,200 ft AGL, and the shear pins that were supposed to hold the main chute inside the rocket broke with the drogue deployment causing the main to be released at apogee, which lost us quite a few points in the competition. However, despite problems with the parachutes leading to minor recovery issues, the overall launch was deemed a success.

Our avionics team began to turn more towards developing custom flight computers, and included a pitot-static tube on the rocket. The propulsion team also made big strides, as this was our first competition rocket that flew on our SRAD solid motor! The payload team impressed the judges and the competition with their first appearance of the two-wheeled rover at an IREC competition.  A bonus payload was on board this year-- an egg! It survived the entire flight without even a minor crack.

2013-2014

In 2013 PROJECT MIDAS was born, which was the name given to the project to the new competition we were participating in: IREC. At this point, we were moving away from USLI as the IREC competition was beginning to grow. The team was growing too, and more than doubled the amount of members to 20 students! The team was excited to make the switch to IREC as it brought with it the promise of being more experimental, in particular it allowed our team to be able to develop our own experimental solid rocket motors in the future.

Project Midas was a 10' tall, 6" diameter vehicle boosted to 10,000' by an Animal Motor Works N2020 White Thunder motor. The airframe was phenolic with a few layers of fiberglass for reinforcement, with fins made out of aluminum. This was also the first time that we made our own parachutes for our rocket.  Meanwhile the payload team continued development of the Rover, however it did not fly during the launch and was instead replaced with balast weight due to issues with received materials a few week before launch. The launch did not go quite to plan, as what appears to be a CATO and following rough landing a left the airframe quite damaged. 

In addition, an ambitious underclassman decided to create our SRAD Propulsion subteam with the help of our Mentor, with the goal of developing SRAD solid rocket motors. The goal was to use this motor at IREC in 2014 to launch our rocket. Characterization testing of our first propellent went decently well (4th/right most image above), the propellant was a difficult consistancy to work with but all four characterization motors performed well, minus the flame being a violet color instead of the desired maroon. A N-class motor was then develop, which immediately CATO'd after ignition as many parts of the motor and closures were ejected out of the aft end. One final attempt at an M-class motor before the competition performed fairly well, however had only around 60% of the desired thrust it was designed for, meaning it was not powerful enough to be used at the competition so an AMW motor was used in it's place. Overall, a great year of learning for the newly formed propulsion subteam! 

2012-2013

This year, the team competed in NASA's USLI Competition. A rough test flight near the competition left the  rocket in a pile of small shards. The payload Rover design was iterated on, first conceptualized and prototyped the year prior. The payload was part of the USLI competition requirements to have a scientific payload, with the goal that the rover would be able to perform scientific experiments on the ground once landed. The team was still very small at this time, having just 9 members. 

2011-2012

The small team began to set their goals high, looking this year to compete in NASA's USLI.  The small group of seniors who had started the team the year prior were able to work with Minnesota Space Grant to sponsor a senior design project, and were later accepted into the competition! There were so many students interested in participating, including students that were not seniors, or from other majors that the university, that the group began to contemplate having a rocketry club as opposed to a senior design group . 

The team worked hard throughout the year to prepare for the NASA competition, conducting a number of scaled test flights, and full-scale test flights as well.  At the competition, we placed mid-pack, with a successful flight which overshot the target altitude. 

Around this time, the team also learned about ESRA's IREC competition, which sparked interest for many members in the group, although the team would not begin competing in IREC until a couple of years later. The summer of 2012 marked the beginning of the effort to move to a club for the following year, instead of a Senior Design group. The new officially formed team was also allocated workspace by the Aerospace Engineering Department in the basement of Akerman hall for the growing rocketry efforts to begin in 2012-2013. 

2010-2011

Back in 2010, an Aerospace Engineering student at the university named Mark Abotossaway attended the American Indian Science and Engineering (AISES) diversity conference in October of 2010. There, he met the organizers of the WSGC First Nations Launch, and knew that he had to find some way to participate. At the time, no one at the University had any experience in rocketry, but was able to form a small team of 5 individuals with the help of Professor Bill Garrard, Director of the Minnesota Space Grant Consortium  at the time, which was the start of our team today. 

The new team started working together in November of 2010 , and a few months later were able to get in touch with a local rocketry expert, Gary Stroick, who then became our team's mentor and remains so to this day. The team had their first test flight in April at the local Tripoli launch site in North Branch, MN, and later won 1st place in the First Nations Launch AISES division!