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{{infobox spaceflight|image=Coin_of_Ukraine_KB_Pivdenne_r.jpg|launch_site=[[Plesetsk Cosmodrome Site 32]]|launch_date=24 December 2004}} |
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'''Sich-1M''' |
'''Sich-1M''' ({{Langx|uk|Січ-1М}}) was a [[Ukraine|Ukrainian]] spacecraft, constructed for [[remote sensing]] of Earth. |
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Designed by [[KB Pivdenne|Yuzhnoye Design Office]] and manufactured by [[PA Pivdenmash|Yuzhmash]]. |
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Sich-1M was launched on December 24, 2004 at 13:20 from the [[Plesetsk cosmodrome]] (Russia) using the [[Tsyklon-3|Cyclone-3]] launch vehicle together with [[MK-1TS]] microsatellite.<ref>{{Cite web|url=http://www.russianspaceweb.com/tsyklon.html|title=Tsyklon-2, 3 {{!}} 11K67, 11K68 {{!}} SL-11, 14, {{!}} F-1, 2|website=www.russianspaceweb.com|access-date=2018-11-13}}</ref> Both satellites placed into incorrect orbits due to premature third stage cutoff. |
Sich-1M was launched on December 24, 2004, at 13:20 from the [[Plesetsk cosmodrome]] (Russia) using the [[Tsyklon-3|Cyclone-3]] launch vehicle together with [[Sich-1M#MK-1TS|MK-1TS]] microsatellite.<ref>{{Cite web|url=http://www.russianspaceweb.com/tsyklon.html|title=Tsyklon-2, 3 {{!}} 11K67, 11K68 {{!}} SL-11, 14, {{!}} F-1, 2|website=www.russianspaceweb.com|access-date=2018-11-13}}</ref> Both satellites were placed into incorrect orbits due to premature third stage cutoff. The satellite remained in orbit until April 15, 2006.<ref>{{Cite web|url=https://www.n2yo.com/satellite/?s=28505|title=Technical details for satellite SICH-1M|website=N2YO.com - Real Time Satellite Tracking and Predictions|access-date=2018-11-13}}</ref> |
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The satellite was in orbit until April 15, 2006.<ref>{{Cite web|url=https://www.n2yo.com/satellite/?s=28505|title=Technical details for satellite SICH-1M|website=N2YO.com - Real Time Satellite Tracking and Predictions|access-date=2018-11-13}}</ref> |
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== Purpose == |
== Purpose == |
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Sich-1M was designed to receive information simultaneously in the optical, [[infrared]] and [[microwave]] ranges. The complex of research equipment installed on the spacecraft allowed to study the [[atmosphere of Earth]] and the [[World Ocean]], monitoring the [[hydrological]] and ice conditions, vegetation and soil cover of the land, etc.<ref>{{Cite journal |doi = 10.1016/S0273-1177(99)00642-0|title = Project VARIANT: Current and field measurements on board SICH-1M satellite|journal = Advances in Space Research|volume = 25|issue = 7–8|pages = 1337–1342|year = 2000|last1 = Korepanov|first1 = V.|last2 = Negoda|first2 = O.|last3 = Lizunov|first3 = G.|last4 = Alleyne|first4 = H.|last5 = Balikhin|first5 = M.|last6 = Blecky|first6 = J.|last7 = Dudkin|first7 = F.|last8 = Fedorov|first8 = A.|last9 = Juchniewicz|first9 = J.|last10 = Klimov|first10 = S.|last11 = Krassnosel'Skikh|first11 = V.|last12 = Lefeuvre|first12 = F.|bibcode = 2000AdSpR..25.1337K|citeseerx = 10.1.1.506.3703}}</ref><ref>{{Cite web|url=http://www.yuzhnoye.com/?id=15&path=about_company/history/spacecraft/spacecraft|title=Главная|website=www.yuzhnoye.com|access-date=2018-11-13}}</ref> |
Sich-1M was designed to receive information simultaneously in the optical, [[infrared]] and [[microwave]] ranges. The complex of research equipment installed on the spacecraft allowed to study the [[atmosphere of Earth]] and the [[World Ocean]], monitoring the [[hydrological]] and ice conditions, vegetation and soil cover of the land, etc.<ref>{{Cite journal |doi = 10.1016/S0273-1177(99)00642-0|title = Project VARIANT: Current and field measurements on board SICH-1M satellite|journal = Advances in Space Research|volume = 25|issue = 7–8|pages = 1337–1342|year = 2000|last1 = Korepanov|first1 = V.|last2 = Negoda|first2 = O.|last3 = Lizunov|first3 = G.|last4 = Alleyne|first4 = H.|last5 = Balikhin|first5 = M.|last6 = Blecky|first6 = J.|last7 = Dudkin|first7 = F.|last8 = Fedorov|first8 = A.|last9 = Juchniewicz|first9 = J.|last10 = Klimov|first10 = S.|last11 = Krassnosel'Skikh|first11 = V.|last12 = Lefeuvre|first12 = F.|bibcode = 2000AdSpR..25.1337K|citeseerx = 10.1.1.506.3703}}</ref><ref>{{Cite web|url=http://www.yuzhnoye.com/?id=15&path=about_company/history/spacecraft/spacecraft|title=Главная|website=www.yuzhnoye.com|access-date=2018-11-13}}</ref> |
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== MK-1TS == |
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<!---use the Ukrainian wiki page @ Мікрон (супутник) to expand---> |
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MK-1TS Micron ({{Langx|uk|МС-1-ТК Мікрон}}) was a small [[Ukraine|Ukrainian]] microsatellite manufactured by [[PA Pivdenmash|Yuzhmash]]. MK-1TS was launched on December 24, 2004, at 13:20 from the [[Plesetsk cosmodrome]] (Russia) using a [[Tsyklon-3|Cyclone-3]] launch vehicle together with the Sich-1M satellite.<ref>{{Cite web |title=Tsyklon-2, 3 {{!}} 11K67, 11K68 {{!}} SL-11, 14, {{!}} F-1, 2 |url=http://www.russianspaceweb.com/tsyklon.html |access-date=2018-11-13 |website=www.russianspaceweb.com}}</ref> Both satellites were placed into incorrect orbits due to premature third stage cutoff. |
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MK-1TS had a small on-board camera (MBTC-VD), to provide digital optical-electronic images in the [[Panchromatic|panchromatic range]].<ref>{{Cite web |title=Мікросупутник дистанційного зондування землі з телевізійною камерою видимого діапазону МС-1-ТК "Мікрон" |url=http://www.nkau.gov.ua/nsau/productnsau2.nsf/add1ac70e70ae1ddc2256c5a0048a80e/9fc829e5e6705c21c2256f40002e661a!OpenDocument |access-date=2018-11-13 |website=www.nkau.gov.ua}}</ref> One of its tasks was to work out a new system of orientation on the base of a [[magnetometer]] and electromagnets without using auxiliary devices.<ref>{{Cite web |title=Аэрокосмический портал Украины / Разработка спутников для дистанционного зондирования Земли |url=http://www.space.com.ua/gateway/news.nsf/NewsALLR/DA5A4E4C78630F8CC2256C36003A233E!open |access-date=2018-11-13 |website=www.space.com.ua}}</ref> The satellite remained active until September 30, 2005.<ref>{{Cite web |title=Technical details for satellite MK-1TS |url=https://www.n2yo.com/satellite/?s=28507 |access-date=2018-11-13 |website=N2YO.com - Real Time Satellite Tracking and Predictions}}</ref> |
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== See also == |
== See also == |
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* [[2004 in spaceflight]] |
* [[2004 in spaceflight]] |
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* [[Sich-1]] |
* [[Sich-1]] |
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* [[Sich-2]] |
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== References == |
== References == |
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Latest revision as of 11:12, 25 October 2024
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| COSPAR ID | 2004-052A |
|---|---|
| SATCAT no. | 28505 |
| Start of mission | |
| Launch date | 24 December 2004 |
| Launch site | Plesetsk Cosmodrome Site 32 |
Sich-1M (Ukrainian: Січ-1М) was a Ukrainian spacecraft, constructed for remote sensing of Earth.
Designed by Yuzhnoye Design Office and manufactured by Yuzhmash.
Sich-1M was launched on December 24, 2004, at 13:20 from the Plesetsk cosmodrome (Russia) using the Cyclone-3 launch vehicle together with MK-1TS microsatellite.[1] Both satellites were placed into incorrect orbits due to premature third stage cutoff. The satellite remained in orbit until April 15, 2006.[2]
Purpose
[edit]Sich-1M was designed to receive information simultaneously in the optical, infrared and microwave ranges. The complex of research equipment installed on the spacecraft allowed to study the atmosphere of Earth and the World Ocean, monitoring the hydrological and ice conditions, vegetation and soil cover of the land, etc.[3][4]
MK-1TS
[edit]MK-1TS Micron (Ukrainian: МС-1-ТК Мікрон) was a small Ukrainian microsatellite manufactured by Yuzhmash. MK-1TS was launched on December 24, 2004, at 13:20 from the Plesetsk cosmodrome (Russia) using a Cyclone-3 launch vehicle together with the Sich-1M satellite.[5] Both satellites were placed into incorrect orbits due to premature third stage cutoff.
MK-1TS had a small on-board camera (MBTC-VD), to provide digital optical-electronic images in the panchromatic range.[6] One of its tasks was to work out a new system of orientation on the base of a magnetometer and electromagnets without using auxiliary devices.[7] The satellite remained active until September 30, 2005.[8]
See also
[edit]
References
[edit]- ^ "Tsyklon-2, 3 | 11K67, 11K68 | SL-11, 14, | F-1, 2". www.russianspaceweb.com. Retrieved 2018-11-13.
- ^ "Technical details for satellite SICH-1M". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2018-11-13.
- ^ Korepanov, V.; Negoda, O.; Lizunov, G.; Alleyne, H.; Balikhin, M.; Blecky, J.; Dudkin, F.; Fedorov, A.; Juchniewicz, J.; Klimov, S.; Krassnosel'Skikh, V.; Lefeuvre, F. (2000). "Project VARIANT: Current and field measurements on board SICH-1M satellite". Advances in Space Research. 25 (7–8): 1337–1342. Bibcode:2000AdSpR..25.1337K. CiteSeerX 10.1.1.506.3703. doi:10.1016/S0273-1177(99)00642-0.
- ^ "Главная". www.yuzhnoye.com. Retrieved 2018-11-13.
- ^ "Tsyklon-2, 3 | 11K67, 11K68 | SL-11, 14, | F-1, 2". www.russianspaceweb.com. Retrieved 2018-11-13.
- ^ "Мікросупутник дистанційного зондування землі з телевізійною камерою видимого діапазону МС-1-ТК "Мікрон"". www.nkau.gov.ua. Retrieved 2018-11-13.
- ^ "Аэрокосмический портал Украины / Разработка спутников для дистанционного зондирования Земли". www.space.com.ua. Retrieved 2018-11-13.
- ^ "Technical details for satellite MK-1TS". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2018-11-13.
External links
[edit]- Space experiment “Variant” onboard SICH-1M satellite (in Ukrainian)
- Sich-1M at eoPortal
- Sich 1M at Gunter's Space Page
- Sich-1M
- SICH, SICH-1M