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Purpose and scope
The development concerns the implementation of the scientific tasks study composition and the ionosphere and thermosphere lower layers state. In particular the study of atomic and molecular oxygen in their composition. The refinement of the atmosphere global ion - thermosphere model
The main characteristics of the development
Weight: 1, 98 kg.
- working condition: 110×100×227 mm;
- transport condition: 675×375×227 mm.
Average power of solar panels: not less than 2. 4 W.
The capacity of the battery: 22 watt - hour.
Maximum short - term energy consumption: 8. 2 W.
The average daily consumption of the satellite (not including FIPEX): 0. 5 W.
Maximum data transfer per day: 0. 3 MB.
Height sun - synchronous orbit above sea level: 412 - 90 km.
Duration of mission: 2 years
State of intellectual property protection
Received 3 patents of Ukraine
Main advantages of the development
The possibility of obtaining valuable orbital telemetry information.
High positioning accuracy using GPS/GLONASS.
Creation of a complete set of equipment (satellite + ground station).
Scalability of the satellite platform in accordance with Cubesat standard.
High computational performance and low power consumption
The work can be useful for enterprises and various forms ownerships industries institutions such as space, emergency, meteorology, ecology, agriculture, etc
Development readiness status
A flight model has been manufactured and launched into orbit. A nanosatellite is operated in orbit