Indian Regional Navigation Satellite System (IRNSS)
IRNSS-1A is the first satellite in the Indian Regional Navigation Satellite System (IRNSS). It is one of the seven satellites constituting the IRNSS space segment.
Payloads - IRNSS-1A carries two types of payloads navigation payload and ranging payload. The navigation payload of IRNSS-1A transmits navigation service signals to the users. This payload is operating in L5-band and S-band. A highly accurate Rubidium atomic clock is part of the navigation payload of the satellite. The ranging payload of IRNSS-1A consists of a C-band transponder which facilitates accurate determination of the range of the satellite. IRNSS-1A also carries Corner Cube Retro Reflectors for laser ranging.
Applications of IRNSS
- Terrestrial, Aerial and Marine Navigation
- Disaster Management
- Vehicle tracking and fleet management
- Integration with mobile phones
- Precise Timing
- Mapping and Geodetic data capture
- Terrestrial navigation aid for hikers and travelers
- Visual and voice navigation for drivers
Lift-off Mass | 1425 kg |
Physical Dimensions | 1.58 metre x 1.50 metre x 1.50 metre |
Orbit | Geosynchronous, at 55 deg East longitude with 29 deg inclination |
Power | Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity |
Propulsion | 440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters |
Control System | Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators |
Mission Life | 10 years |
Launch date | Jul 01, 2013 |
Launch site | SDSC SHAR Centre, Sriharikota, India |
Launch vehicle | PSLV - C22 |
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