| Mission type | Ionosphere research |
|---|---|
| Operator | State Space Agency of Ukraine |
| Website | "Ionosat-Micro" Mission |
| Spacecraft properties | |
| Spacecraft | "Mikrosat-M"[1] |
| Manufacturer | Yuzhnoye State Design Office |
| Launch mass | 200 kilograms (440 lb) |
| Payload mass | 75 kilograms (165 lb) |
| Expedition | |
| Began | 2020s |
| Orbital parameters | |
| Reference system | Circular Solar-synchronous |
| Regime | Low Earth |
| Inclination | 97,9…98,2° |
| Argument of periapsis | 620–710 kilometres (390–440 mi) |
Ionosat Micro is a Ukrainian satellite mission.[2]
The head scientific organization is the Space Research Institute of NAS of Ukraine and SSA of Ukraine.
General information
"Ionosat-Micro" Mission realized under the National purpose scientific and technical space program of Ukraine.
Particular project tasks:
Project partners
| Organizationation | Part in the project | |
|---|---|---|
| UKRAINE | ||
| Space Research Institute of National Academy of Sciences of Ukraine and State Space Agency of Ukraine (SRI), Kyiv | Coordination of research program. Maintenance of functioning of the Data processing, storage and distribution center PROMIS | |
| Yuzhnoye State Design Office, Dnipro | Spacecraft «Microsat-M» designing and launch, payload integration, spacecraft operation planning, formation of accompanying information on spacecraft parameters | |
| Lviv Centre of Space Research Institute, Lviv | Onboard scientific instrumentation integration. Creation of instruments: MWC, ODHS and electronic unit of PDA. Measurement realization and data processing | |
| Institute of Technical Mechanics, Dnipro | DN and DE sensors creation, measurement realization and data processing | |
| National Center of Space Facilities Control and Test | Flight control. Telemetry and scientific information receiving from the spacecraft | |
| POLAND | ||
| Space Research Center, Warsaw | Instrument RFA creation, measurement realization and data processing | |
| BULGARIA | ||
| Space Research and Technology Institute, Sofia | Instrument ID-2 creation, measurement realization and data processing | |
The history of the project
Formation of the scientific objectives of the project "Ionosat - Micro" was for a long time, and conceptual provisions were first formulated in the 1990s, during the development of unrealized mission "Warning." Then, after tragic Spitakskii earthquake (1988), the political leadership of the USSR initiated the development of new, more effective methods of earthquake prediction, based, in particular, on the use of non-traditional for Seismology approaches such as observation of ionospheric harbingers of earthquakes etc. Thus arose the idea of mission "Warning", which, if not collapse of the USSR (1991), could be the most ambitious satellite project in the history of world studies of the ionosphere. The "Ionosat-Micro" Mission on the satellite "Mikrosat-M" embodies the ideas of the mission "Warning" on modern scientific and technological basis.[3][4]
For the diagnosis of electromagnetic processes in ionospheric plasma in the "Ionosat-Micro" Mission will be used complex instrument MWC, developed by Lviv Centre of Space Research Institute. Experimental testing elements MWC was conducted space experiments "Variant" in the Ukrainian remote sensing satellite "Sich-1M" (2004).[5] To measure the parameters of the ionosphere gas - concentration and temperature neutral and ionized gases - is a complex instrument DN - DE, established in Institute of Technical Mechanics. Flight testing sensors DN and DE experiment was carried out in "Potential" in the Ukrainian remote sensing satellite Sich-2 (2012).[6] In the "Ionosat-Micro" Mission involving foreign partners: Space Research Center of the Polish Academy of Sciences (translated) is instrument RFA creator and Space Research and Technology Institute is instrument ID-2 creator.
The satellite launch was planned for 2018. As of May 2019, work is go on.[7]
Spacecraft and orbit
"Ionosat-Micro" scientific instrumentation set is installed on the satellite platform «Microsat-M» [8] designed by Yuzhnoye State Design Office to conduct scientific and technological experiments. Ideas for the satellite launching into orbit are processed.
| ORBIT | ||
|---|---|---|
| Circular, the operating range of heights | 620...710 km | |
| Inclination | 97,9...98,2° | |
| Solar-synchronous, local time in a descending node | 10...14 hours | |
| ORIENTATION | ||
| type | active three axes | |
| orientation error in the orbital coordinate system | not more than 5° (3σ) | |
| angular rate of spacecraft stabilization | not more than 0,01 °/с (3σ) | |
| DATA TRANSMISSION TO THE EARTH | ||
| X-range radio line | 30.72 Mbit/s | |
| S-range service radio line | 32 kbit/s | |
| SPACECRAFT WEIGHT | ||
| total | up to 200 kg | |
| payload | up to 75 ky | |
| WARRANTY PERIOD | ||
| not less than 3 years | ||
| SPACE AND TIME MEASUREMENTS ERRORS | ||
| spacecraft positioning error | not more than 1.5 km | |
| spacecraft orientation error (sensors axes) | not more than 1° | |
| onboard time scale error | not more than 1 msec | |
"Ionosat-Micro" scientific instrumentation
Scientific instrumentation onboard "Microsat-M" designation:
General characteristics of «Ionosat-Micro» scientific instrumentation set:
- weight < 20 kg
- power consumption < 51 W
- data downstream up to 6 GB per day
«Ionosat-Micro» scientific instrumentation set:
Sources
- ↑ (eng) Mikrosat — Yuzhnoye Design Office
- ↑ "(ru) Лизунов Г.В., Лукенюк А.А., Макаров А.Л., Фёдоров О.П. Космический проект «Ионосат – Микро»: цели и методы // Космический проект «Ионосат-Микро»: монография / Под общ. ред. С.А. Засухи, О.П. Фёдорова. – К.: Академпериодика, 2013. – С. 11–25". Archived from the original on December 21, 2016. Retrieved December 15, 2016.
- ↑ (ukr) Лізунов Г.В. Українські супутникові проекти іоносферних спостережень: від «Попередження» до «Іоносату» // Світогляд. – 2014. – №6 (50). – С. 18–24
- ↑ (eng) Korepanov V., Lizunov G., Fedorov O., Yampolsky Yu., Ivchenko V. Ionosat – ionospheric satellite cluster // Adv. Space Res. – 2008. – V. 42. – P. 1515—1522
- ↑ (eng) Dudkin F., Korepanov V., Lizunov G. Experiment VARIANT – first results from wave probe // Adv. Space Res. − 2009. − V. 43. − P. 1904−1909
- ↑ (eng) Makarov O.L., G.V. Lizunov, A.A. Lukeniuk, V.Ye. Korepanov, V.O. Shuvalov, Yu.A. Shovkoplias, S.I. Moskalev. Experiment POTENTIAL onboard SICH-2 microsatellite – first results // 63rd International Astronautical Congress, Naples, Italy, October 1–5, 2012. IAC-12-B4.2.13571
- ↑ "В Украине разрабатывают четыре типа новых спутников". May 10, 2019.
- ↑ (ru) Макаров А. Л., Шовкопляс Ю.А., Москалев С.И., Галабурда Д.А. Космический аппарат «Микросат» // Космический проект «Ионосат-Микро»: монография / Под общ. ред. С.А. Засухи, О.П. Фёдорова. – К.: Академпериодика, 2013. – С. 109—117