There are several raw ideas about Orbita 2.0 (earth model) missions. For instance, the telecom satellite mission:
Your mission is to develop a satellite communications system providing the service of two-way access to the Internet. The satellite must be designed for placement on the geostationary orbit, carry 24 Ku-band transponders, have a launch mass of no more than 3200 kg, the power supply system at the end of active life must be at least 5 kW. The ground station uses parabolic antenna with a diameter of 0.75 meters. The design should minimize the cost of the space segment of the system, the cost of ground subscriber terminal and the cost of system services.
The new missions need to be designed, implemented in missions.xml file and the mission evaluation script, model documentation, and tested with different cases.
There are several raw ideas about Orbita 2.0 (earth model) missions. For instance, the telecom satellite mission:
Your mission is to develop a satellite communications system providing the service of two-way access to the Internet. The satellite must be designed for placement on the geostationary orbit, carry 24 Ku-band transponders, have a launch mass of no more than 3200 kg, the power supply system at the end of active life must be at least 5 kW. The ground station uses parabolic antenna with a diameter of 0.75 meters. The design should minimize the cost of the space segment of the system, the cost of ground subscriber terminal and the cost of system services.
The new missions need to be designed, implemented in missions.xml file and the mission evaluation script, model documentation, and tested with different cases.