MOS-1 (satellite)
Marine Observation Satellite-1 (MOS-1), also known as Momo-1, was Japan's first Earth observation satellite. It was launched on 19 February 1987 on a N-II rocket from Tanegashima Space Center and was operated by the National Space Development Agency of Japan (NASDA). It is in a polar orbit at roughly 900 km altitude, but has been decommissioned on 29 November 1995.
| Names | MOS-1, Momo-1 | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mission type | Earth observation | ||||||||||
| Operator | NASDA | ||||||||||
| COSPAR ID | 1987-018A | ||||||||||
| SATCAT no. | 17527 | ||||||||||
| Mission duration | Planned: 2 years Final: 8 years, 9 months, 9 days | ||||||||||
| Spacecraft properties | |||||||||||
| Manufacturer | NEC [1] | ||||||||||
| Launch mass | 750 kg [2] | ||||||||||
| Start of mission | |||||||||||
| Launch date | 19 February 1987 01:23:00 UTC [3] | ||||||||||
| Rocket | N-II (N-16F) [4] | ||||||||||
| Launch site | Tanegashima LC-N | ||||||||||
| Contractor | NASDA | ||||||||||
| End of mission | |||||||||||
| Disposal | Decommissioned | ||||||||||
| Deactivated | 29 November 1995 | ||||||||||
| Orbital parameters | |||||||||||
| Reference system | Geocentric | ||||||||||
| Regime | Sun-synchronous | ||||||||||
| Perigee altitude | 909 km [5] | ||||||||||
| Apogee altitude | 909 km | ||||||||||
| Inclination | 99.1° | ||||||||||
| Period | 103.2 minutes | ||||||||||
| |||||||||||
Instruments
It has four instruments:
- "Multi-Spectral Electronic Self-Scanning Radiometer (MESSR)" which offers 50 m resolution in two visible and two infra-red spectral bands over two 100 km swathes.
- "Visible and Thermal Infrared Radiometer (VTIR)" which has a much lower resolution in one visible and three infrared bands over a 1,500 km swathe.
- "Micro Scanning Radiometer (MSR)" which measures microwave emission in the 23 GHz and 31 GHz bands.
- "Data Collection System (DCS)" which is an experimental transponder.[7]
References
- Ninomiya, Keiken (2005). Nebylov, Alexander (ed.). Automatic Control in Aerospace 2004. Proceedings of the 16th IFAC Symposium, Volume 1. Elsevier. p. 199. ISBN 0-08-044013-4.
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
- https://global.jaxa.jp/projects/rockets/n2/index.html
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020
External links
- MOS-1 site by JAXA
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.