The ECE3SAT project is a student project developed at the french engineer school, ECE Paris . The goal of the project is to send a Cubesat in space to verify a physical theory permitting a fast deorbiting. The ECE3SAT is composed of five modules named Attitude Determination Control System (ADCS) Energy Power Supply (EPS) On Board Computer (OBC) Payload (PAYLOAD) Telecommunication System (TCS) The Cubesat development is divided in five different phases, 0, A, B, C & D and E & F. Each phase is supposed to be realized in 1 Year. The goal of the project is to succeed in the mission, but also to enable students to overcome a physical theory through the realization of a satellite.
| Website | http://www.ece3sat.com/ |
| Employees | 1 (0 on RocketReach) |
| Keywords | Cubesat, Cubesat Development, Spacecraft, Satellite, Space Technology, Satellite Technology, Aerospace, Space Research, Orbital Mechanics, Engineering, Experimental Physics, Research, Technology, Science |
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