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It is capable of launching mini, micro or nano satellites (10 to 500 kg mass) into 500 km planar orbit.
SSLV is a three-stage launch vehicle with all solid propulsion stages and liquid propulsion based Velocity Trimming Module (VTM) as terminal stage.
Design drivers of SSLV are low cost, low turn-around time, flexibility in accommodating multiple satellites, launch on demand feasibility, minimal launch infrastructure requirements, etc.
SSLV-D3 is the third developmental flight of SSLV.
The EOS-08 is an Earth Observation Satellite built on ISRO’s Microsat/IMS-1 bus platform. It is designed to operate in a circular Low Earth Orbit (LEO) at an altitude of 475 km and has a mission life of one year.
Electro Optical Infrared Payload (EOIR): The EOIR captures images in the Mid-Wave Infrared (MIR) and Long-Wave Infrared (LWIR) bands. It operates day and night, supporting applications like satellite-based surveillance, disaster and environmental monitoring, fire detection, volcanic activity tracking, and industrial disaster monitoring.
Global Navigation Satellite System — Reflectometry (GNSS-R) Payload: The GNSS-R payload demonstrates remote sensing using GNSS-R for applications like measuring ocean surface winds, detecting soil moisture, monitoring the Himalayan cryosphere, and identifying floods and inland water bodies.
SiC UV Dosimeter: The SiC UV dosimeter measures UV radiation.
The EOS-08 satellite includes an Integrated Avionics System that combines communication, baseband, storage, and positioning (CBSP) functions.
It also has a structural panel with an embedded printed circuit board (PCB) and battery.
The successful launch of SSLV-D3 and the precise orbit placement of the EOS-08 satellite are major milestones for ISRO.
This mission enhances India’s Earth observation abilities and showcases new advancements in satellite technology.
By: Shubham Tiwari ProfileResourcesReport error
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