// Workers AI · dad joke modeWhat did SRMSAT say to its friend? You're a sat-ellite friend.
| Mission type | Technology |
|---|---|
| Operator | SRM Institute of Science and Technology |
| COSPAR ID | 2011-058D |
| SATCAT no. | 37841 |
| Website | www |
| Mission duration | 12 months (planned) 14 years, 9 months, 13 days (in progress) |
| Spacecraft properties | |
| Launch mass | 10 kilograms (22 lb) |
| Start of mission | |
| Launch date | 12 October 2011 |
| Rocket | PSLV C18 |
| Launch site | Satish Dhawan FLP |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Inclination | 20 degrees |
| Period | 102.1 minutes |
| |
SRMSAT is a Nanosatellite built by faculty and students at Sri Ramaswamy Memorial University (SRM Institute of Science and Technology, Chennai) in India. The satellite is an Indian Technology demonstration and Earth observation satellite which is operated by the SRM Institute of Science and Technology. This nanosatellite was used to monitor Greenhouse gases in atmosphere.
SRMSAT's primary mission was the development of a nanosatellite platform for future missions. Its secondary mission was monitoring of greenhouse gasses[1] using an Argus Spectrometer.[2]
Specifications
[edit]- It is a 10.4-kilogram (23 lb) spacecraft, which measures 28 centimetres (11 in) in length by 28 centimetres (11 in) in height and width.
- Its development programme cost around 1.5 crore rupee.
- It had a design life of one year, but is still working As of October 2017[update] and can be tracked easily on n2yo.com [3]
Launch
[edit]It was launched from the Indian Space Research Organisation (ISRO)'s Satish Dhawan Space Centre at Sriharikota in October 2011.[4] atop a Polar Satellite Launch Vehicle (PSLV) C18 rocket. The launch was a multi-payload mission shared with Megha-Tropiques, VesselSat-1 and Jugnu.[5]
Parameters
[edit]SRMSAT[6] is controlled by a 28.8 MHz Atmel microcontroller. Communication is via Ultra high frequency (UHF), with a downlink at 437.5 MHz providing a data rate of 2.4 kbit/s and an uplink at 145.9 MHz with a 1 kbit/s data rate. Attitude control is via solar cell management system (SCDM), an on-board magnetometer and Global Positioning System (GPS) receiver that provide data for magnetorquer coils which interact with the Earth's magnetosphere to change the satellite's orientation.[citation needed]
See also
[edit]
References
[edit]- ↑ "TN university plans centre for space technology". The Times of India.
{{cite web}}: CS1 maint: deprecated archival service (link) - ↑ "Argus Infrared Spectrometers". Thoth Technology Inc. Archived from the original on 27 November 2013.
- ↑ "LIVE REAL TIME SATELLITE TRACKING AND PREDICTIONS: SRMSAT". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 28 October 2015.
- ↑ "PSLV-C18 carrying weather satellite launched". Times Of India.
- ↑ Subramanian, T. S. (12 October 2011). "PSLV-C18 puts four satellites in orbit". The Hindu. Retrieved 26 January 2012.
- ↑ "SRMSAT". NASA.
External links
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