We design a non-androgynous type, universal Assembly/Docking Device that could be used for put together two structures in space, it is useful for docking space vehicles as well as structures or modules, like the ones that are planned for "The Gateway".
This development is key to set up in space small satellites, medium spacecrafts and big structures (telescopes, space station modules, etc).
This device is composed by two subsystems: Male part (active) and Female part (passive).
The male part, it´s integrated by a electrical motor, an endless piston, and a ball joint at the end of it. (The motor is inside de the blue box).
The female part it´s made of a conical shaped mechanism, with a set of 4 electromagnets and a 4 springs in each side of the device.

Female Cover

This device works as follows: The electrical motor in the male part (mounted in space vehicle A) moves the endless piston forward until it reaches the docking station (mounted in space vehicle B) and the ball joint passes through the 4 "petals" of the female part, while the springs blocks any movement . Also the electrical motor, blocks any further movement of the piston, but if it´s needed, the powerful motor could generate backwards movement of the piston, "attracting" the spacecraft B to the spacecraft A.
If we want to release the female part, we activate the electromagnets and the petals will opens, because the electromagnetic force will be greater than the force of the springs.
Also in certain structures, as hotels or telescopes that doesn´t need to "unmount", our female part, won´t need the electromagnetic open array, and it could be suppressed.

The achievements we wanted to reach, were a universal, simple, secure and low cost device for both docking and assembling, making possible a fastest way to build things in space.
We choose the project motivated by a strong conviction to make a real change in how space operations are done, and contribute to solve a real problem.
Our approach was a qualitiative analysis of the requirements that all the system for docking and assembling has to have.
Firstable we analyzed the state of the art in docking and assembling systems and also the space constraints affecting materials in space, that information was extracted from NASA Databases and research repositories, then we started with a prototype designed in SolidWorks, but when we tried to perform the "proof of concept" of our design, we discovered that we have to rethink our approach.
Also we received feedback from the experts of our local challenge on what kind of material we need to use in order to make stronger our endless piston, because of the stress that the docked/assembled structures will be suffering. And the we decided to change Aluminium 2024 for an Aluminium and titanum alloy.
NASA Databases
Canadian Space Agency from the NASA space apps page (including a space material database)
They were very useful because we could gather all the scientific facts in order to see how it affects our design.
As well as find out the real NASA projects and challenges faced now and in the near future. We did research for every decision and step taken.
We can said that our approach to the project was influenced by this data because we adapted our initial design to get our final product. Also we could perfom a material analysis to find the right option for our project.
References
