Youth for Space Challenge – ODYSSEUS II Contest Project Worksheet 1 Pi-Mars In order to summarize and highlight the key aspects of your entry to the Odysseus II Contest, you are advised to submit alongside your Project, the Project Worksheet that you will find below. Please take into consideration the following suggestions in order to complete the Worksheet correctly and enable the evaluators to better understand the scope and methodology of your work. Be aware that the parts of the Worksheet correspond to the assessment criteria. All parts of this form must be filled. The Odysseus II Contest project worksheet could be completed in any EU official language. Enter your text in the respective boxes provided in each section. The overall content of the worksheet should not exceed 3,000 words (excluding literature references). The maximum length of each section is shown in the beginning of the section. Replace the footer “Title of the project” with the title of your project. Write the category you are competing in along with the name of your team (if you compete in the Pioneers category). In all boxes remove the guidelines before adding your text. Good Luck! 2 Pi-Mars Project Title: .......Pi-Mars......................................................... Topic in which the entry is submitted: Space Science....................................................................................................... Team Name: Pi Explorers..................................................... (for Pioneers category) Contestant’s Name(s): ...................................................... (for Explorers category) Abstract (max. 400 words) We have chosen to do this project because one main reason: the cost our project is small compared to other major projects, such as the Curiosity Rover. Our idea is to drop more of our modules on Mars Surface, to measure parameters which would eventually help astronauts find out conditions on Mars in a fast manner. This project contains all the instructions for building our module, such as guidance for the space capsule's dimensions and total cost. We have also included the computation of atmospheric speed and total mass of the module. We expect that our module is very competitive because of these reasons (including building availability). Key Concept of the project Perhaps the most important advantage of our project is the price necessary to achieve it, about 150 USD. In comparison to other projects, such as Curiosity rover, we manage to obtain scientific results such as temperature, 3 Pi-Mars humidity and pressure on Mars, at a very low price. The purpose of obtaining them is to ensure that astronauts who will land on the planet will be in optimal conditions and that devices used will withstand in the condition of live monitoring. Also, on the way to Mars in the Atlas V rocket we will measure those parameters and show them live to avoid a disaster. Methodology for implementation Pi, which is powered by a 10000 mAh battery, after it has been deployed. Also, all its 40 pins are used to connect to the Top Hat module, that has a 8x8 led matrix, and humidity, temperature, and pressure sensors attached to it. Our main test concluded to poll the values of the humidity, temperature, and pressure every second, and to mark down the values for further evaluation. In the first tests after writing and debugging the code, we wanted to see if our sensors were working properly, and to analyse how would the Up-Time of the Raspberry Pi was affecting out results. Judging by the fact that our Raspberry Pi doesn’t have a heatsink, and by the results of the test, we concluded that we have to run our tests as close to power-up for optimal results, as processor-made heat cannot be ventilated, and it could affect our readings (a ventilator might drop our registered temperatures). In the next test we wanted to see how a quick increase in temperature would affect the other sensors’ readings, by using a hairdryer. The humidity started to drop, 4 Pi-Mars and the pressure stood at a normal level. We also realized that the temperature was an indicator of how far the hairdryer was from the Raspberry Pi board. This simulation showed us how would temperature change in the Atlas V module, but also during the drop. Social Relevance The current social relevance is the fact that our module would be available at a very cheap price tag, and it could even be used on Earth, without the capsule, of course. This would have a major impact on the modern society, as almost everyone would afford this device. Sustainability The sustainability of our planet would be improved, because our module helps people gain information about many parameters, and the general quality of the environment. This would lead to a major attitude change from the people, who would become more responsible here on Earth, and possibly, on Mars. 5 Pi-Mars Findings and conclusions We did carry out a couple of tests, from which two are detailed below: - We exhaled air over the sensors for 10 seconds, with 2 seconds between each measuring, concluding that the humidity rose very fast, while the temperature started to rise noticeably. Number/Sensor Humidity Temperature Pressure 1 45.3904 23.2063 1014.6569 2 48.6330 23.2816 1014.6564 3 54.2479 23.5416 1014.6479 4 61.9427 23.7060 1014.6745 5 67.4297 23.8512 1014.6569 - We blew hot air over the sensors for 5 seconds, with one second between each measuring, concluding that the humidity started to go down, while the temperature rose steadily. Number / Sensor Humidity Temperature Pressure 41.2604 31.8199 1011.1152 1 2 41.0856 31.8199 1011.1152 3 40.8965 32.3494 1011.1040 4 40.8073 32.8425 1011.1430 5 40.5396 32.8790 1011.1386 Such measurements should provide accurate weather predictions, such as storms or droughts on Mars. 6 Pi-Mars References https://ro.wikipedia.org/wiki/Constanta_gravita%C8%9Bional%C 4%83 https://ro.wikipedia.org/wiki/Legea_atrac%C8%9Biei_universale https://en.wikipedia.org/wiki/Drag_coefficient https://en.wikipedia.org/wiki/Atmosphere_of_Mars https://en.wikipedia.org/wiki/Mars http://www.engineeringtoolbox.com/drag-coefficient-d_627.html 7 Pi-Mars
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