Science & Technology Current Affairs Analysis
ISRO to launch earth observation satellite on Independence Day
Context:
The Indian Space Research Organisation (ISRO) will commemorate Independence Day by launching an Earth Observation Satellite (EOS).
ØThe satellite will be launched using a Small Satellite Launch Vehicle (SSLV).
About EOS-08 mission:
EOS-08 is ISRO’s latest Earth Observation Satellite, slated for launch by the Small Satellite Launch Vehicle (SSLV)-D3.
The primary objectives of the EOS-08 mission include designing and developing a microsatellite, creating payload instruments compatible with the microsatellite bus, and incorporating new technologies required for future operational satellites.
Built on the Microsat/IMS-1 bus, EOS-08 carries three payloads:
1Electro Optical Infrared Payload (EOIR),
2Global Navigation Satellite System-Reflectometry payload (GNSS-R), and
3SiC UV Dosimeter.
ØThe EOIR payload is designed to capture images in the Mid-Wave IR (MIR) and Long-Wave IR (LWIR) bands, both during the day and night.
§Applications : satellite-based surveillance, disaster monitoring, environmental monitoring, fire detection, volcanic activity observation.
ØThe GNSS-R payload demonstrates the capability of using GNSS-R-based remote sensing for applications such as ocean surface wind analysis, soil moisture assessment, cryosphere studies over the Himalayan region, flood detection, and inland waterbody detection.
ØThe SiC UV Dosimeter monitors UV irradiance at the viewport of the Crew Module in the Gaganyaan Mission and serves as a high-dose alarm sensor for gamma radiation.
The spacecraft mission configuration is set to operate in a Circular Low Earth Orbit (LEO) at an altitude of 475 km.
The satellite employs a miniaturized design in its Antenna Pointing Mechanisms, capable of achieving a rotational speed of 6 degrees per second and maintaining a pointing accuracy of ±1 degree.
About Small Satellite Launch Vehicle (SSLV)
Small Satellite Launch Vehicle (SSLV) is a three stage Launch Vehicle configured with three Solid Propulsion Stages and a liquid propulsion-based Velocity Trimming Module (VTM) as a terminal stage.
ØSSLV is 2m in diameter and 34m in length with a lift-off weight of around 120 tonnes.
ØSSLV is capable of launching 500kg satellites in 500km planar orbit from Satish Dhawan Space Centre (SDSC).
Key Features:
ØLow cost,
ØLow turn-around time,
ØFlexibility in accommodating multiple satellites,
ØLaunch demand feasibility,
ØMinimal launch infrastructure requirements, etc.
Earlier, the bigger satellite payloads were given importance, but as the sector grew many players emerged like Businesses, government agencies, universities, and laboratories began to send satellites.
ØMostly all of them fall in the category of small satellites.
Types of orbits:
High Earth Orbit (HEO)
HEO liesat and beyond 35,786 kilometersfrom Earth’s surface. It is a sort of “sweet spot” in which satellite orbit matches the rotation of the Earth.
Medium Earth Orbit (MEO)
MEO lies between 2,000 km to 35780 km from the surface of the Earth. Two Medium Earth Orbits are the semi-synchronous orbit and the Molniya orbit. MEO satellites have orbital periods ranging from 2 to 24 hours. Satellites in MEO have an orbital period between 2 to 24 hours.
Low Earth Orbit (LEO)
LEO has an altitude between160 km to 1000 kmabove the Earth’s surface. Satellites in this orbit take approximately88 - 127 minutesto circle Earth.