Bringing Home the Argonia Cup—Again!
A successful two-stage launch, in which the stages fully separate in flight, is hard to achieve. The main challenge is getting the second motor to ignite properly in flight. To do this, we used redundant timer-based ignition systems that also have tilt limits. The tilt limits make sure the second stage doesn’t ignite if the rocket is tilted by more than 20 degrees from vertical. Two-stage rockets also require twice as many electronics for recovery and deployment as single-stage rockets, and two-stage launches have more uncertainty. Further, the mechanical coupling between the two stages is full of opportunities for failure, including early and late release.
We planned to deliver the payload (the golf ball) to the X using a small quadcopter deployed by the rocket at its highest altitude. Using a rocket with a small diameter meant that we needed a small drone (quadcopter). We wanted a drone with 3-inch-diameter propellers that could hold a large battery yet fit into a 2.6-inch-diameter rocket (the propellers are linear and fit in the rocket tube lengthwise). So, we designed one. We ran into a few problems, but we were able to mitigate them.
At the Argonia Cup we were the only team to meet all the requirements of the competition: landing the golf ball and recovering all parts of the rocket in working condition. So, despite landing our golf ball 2.41 miles away from the X and a score of about -239,000 feet (yes, negative!), we still won the competition.
We’re now preparing for the 2024 challenge, to get the highest score calculated by A*((N/10) + 1) with a two-stage rocket, where A is the height (in feet) of the upper stage (sustainer) at apogee, and N is the number of golf balls carried in the sustainer. The total impulse of the motors must be less than or equal to 5120 Newton-seconds. See you at the competition!
The Rocket Dawgs are supported by Madeline Baugher and the Oklahoma NASA