Back in October 2016, two students from DHBW Stuttgart reached out to us because they needed help with a graduation project. The goal was to build a water rocket which collects data from the environment such as particulate matter, carbon dioxide, atmospheric humidity and much more. During our first meeting in a restaurant we decided to help them and made the first steps in developing a concept for the project. But we didn‘t want to build just a water rocket and put the electronics in it - we wanted to go a step further and develop something new:
THE CONCEPT
The plan was to place a mechanism on top of a modified „Ueberflieger Mini Evo“ Water Rocket, which should eject the upper part of the rocket (including the electronics) right after reaching the apogee. This enables the sensors to collect much more data than on a regular flight without probe ejection since the probe has a pretty large parachute.
During the construction we faced numerous problems. The probe had to have a sufficient spring in order to separate it from the rocket. But at the same time, the mechanism had to be strong enough to prevent the probe to be ejected before reaching the apogee. The connection between probe and rocket was planned to consist of a shrunken bottle (in hot water), but unfortunately it turned out that the rubber bands pressed the probe so strong against the connection that the spring wasn‘t able to eject the probe anymore. After some prototyping, we were able to solve the problem with a new connection which has a stop point, so the probe and the rocket were not able to stick together anymore.
VIDEO
parachute
probe
spring
nozzle withopening for the air duct
power supply
air duct
lower base plate
upper base plate
case
rods
sensors
prototyping
inner structure of the probe
ejection mechanism
CONSTRUCTION OF THE PROBE
The separation of the probe and the water rocket should be realized with a tommy timer, just like our regular parachute mechanisms work. This was really challenging because the rubber band had to be deflected two times at the probe. The timer itself is placed at the ejection mechanism, not at the probe.
LAUNCH
On March 26th, we were finally ready to launch the rocket with the probe. The day started with the assembly of the last components and some ground tests. In the early afternoon, we set out to launch the rocket. But that didn‘t turned out well: Due to a damage on one of the bottles, the upper segment of the rocket exploded at 14 bar / 200 psi. Luckily, the damage wasn‘t as bad as expected. Only the ejection mechanism had to be rebuilt. And so we were able to start a second attempt of launching the rocket in the evening…
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PROJECT EOWREARTH OBSERVATION WATER ROCKET
Back in October 2016, two students from DHBW Stuttgart reached out to us because they needed help with a graduation project. The goal was to build a water rocket which collects data from the environment such as particulate matter, carbon dioxide, atmospheric humidity and much more. During our first meeting in a restaurant we decided to help them and made the first steps in developing a concept for the project. But we didn‘t want to build just a water rocket and put the electronics in it - we wanted to go a step further and develop something new:
THE CONCEPT
Fallschirm
Sonde
Feder
nozzle withopening for the air duct
power supply
air duct
lower base plate
upper base plate
case
rods
sensors
CONSTRUCTION
prototyping
inner structure of the probe
ejection mechanism
THE LAUNCH
VIDEO
The plan was to place a mechanism on top of a modified „Ueberflieger Mini Evo“Water Rocket, which should eject the upper part of the rocket (including the electronics) right after reaching the apogee. This enables the sensors to collect much more data than on a regular flight without probe ejection since the probe has a pretty large parachute.
The separation of the probe and the water rocket should be realized with a tommy timer, just like our regular parachute mechanisms work. This was really challenging because the rubber band had to be deflected two times at the probe. The timer itself is placed at the ejection mechanism, not at the probe.
During the construction we faced numerous problems. The probe had to have a sufficient spring in order to separate it from the rocket. But at the same time, the mechanism had to be strong enough to prevent the probe to be ejected before reaching the apogee. The connection between probe and rocket was planned to consist of a shrunken bottle (in hot water), but unfortunately it turned out that the rubber bands pressed the probe so strong against the connection that the spring wasn‘t able to eject the probe anymore. After some prototyping, we were able to solve the problem with a new connection which has a stop point, so the probe and the rocket were not able to stick together anymore.
On March 26th, we were finally ready to launch the rocket with the probe. The day started with the assembly of the last components and some ground tests. In the early afternoon, we set out to launch the rocket. But that didn‘t turned out well: Due to a damage on one of the bottles, the upper segment of the rocket exploded at 14 bar / 200 psi. Luckily, the damage was not as bad as expected. Only the ejection mechanism had to be rebuilt. And so we were able to start a second attempt of launching the rocket in the evening…