Mikhailo Lomonosov (satellite)
Mission type | Astronomy |
---|---|
Operator | MSU |
COSPAR ID | 2016-026A |
SATCAT № | 41464 |
Mission duration | Planned: 3 years[1] |
Spacecraft properties | |
Manufacturer | VNIIEM |
Launch mass | 620 kg (1,370 lb)[1] |
Payload mass | 170 kg (370 lb)[1] |
Power | ~300 W[1] |
Start of mission | |
Launch date | 28 April 2016, 02:01 UTC (planned) |
Rocket | Soyuz-2.1a/Volga |
Launch site | Vostochny Site 1S |
Contractor | Roscosmos |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Semi-major axis | 6,856 kilometers (4,260 mi)[2] |
Perigee | 478.2 km (297.1 mi)[2] |
Apogee | 492.9 km (306.3 mi)[2] |
Inclination | 97.3 degrees[2] |
Period | 94.2 minutes[2] |
Instruments | |
List
|
Mikhailo Lomonosov (or MVL-300) is an astronomical satellite of MSU named after Mikhail Lomonosov.[3]
Mission
The objective of the mission is the observation of gamma-ray bursts, high-energy cosmic rays and transient phenomena in the Earth's upper atmosphere.[3]
One of the instruments on board is the TUS (Tracking Ultraviolet Set Up) system, which is designed to measure fluorescence light radiated by EAS (Extensive Air Showers) of Ultra High Energy Cosmic Rays (UHECR) in the earth atmosphere as well as for transients’ studies within UV-range.[4]
For studying gamma-ray bursts Lomonosov has UFFO and BDRG instruments.
References
- 1 2 3 4 "Космический аппарат «Ломоносов»" (in Russian). Retrieved 21 March 2016.
- 1 2 3 4 5 "MVL 300 Satellite details 2016-026A NORAD 41464". N2YO. 4 May 2016. Retrieved 4 May 2016.
- 1 2 "Soyuz prepared for first flight from Siberian cosmodrome". Spaceflight Now. Retrieved 21 March 2016.
- ↑ "MVL-300 (Mikhailo Lomonosov)". Gunter's Space Page. Retrieved 21 March 2016.
External links
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