Understanding ISRO's evolution from experimental sounding rockets to heavy-lift launch vehicles and cryogenic engines.
- PSLV (Polar Satellite Launch Vehicle): Known as the 'Workhorse of ISRO', it is a 4-stage launch vehicle alternating solid and liquid fuel stages (Solid-Liquid-Solid-Liquid). It is primarily used for Sun-Synchronous Polar Orbits (SSPO) and remote sensing satellites.
- GSLV (Geosynchronous Satellite Launch Vehicle): A 3-stage heavy-lift vehicle featuring a solid first stage, liquid second stage, and an indigenous cryogenic upper stage (CE-7.5 or CE-20). Designed for placing communication satellites into Geostationary Transfer Orbit (GTO).
- LVM3 (Launch Vehicle Mark 3 / GSLV Mk III): ISRO's heaviest operational rocket featuring two solid strap-on boosters (S200), a core liquid stage (L110), and a high-thrust cryogenic upper stage (C25). Successfully deployed Chandrayaan-2, Chandrayaan-3, and OneWeb commercial payloads.
- Cryogenic Technology: Utilizes liquid hydrogen (LH2 as fuel at -253°C) and liquid oxygen (LOX as oxidizer at -183°C). Provides significantly higher specific impulse compared to solid and earth-storable liquid propellants.
- SSLV (Small Satellite Launch Vehicle): Designed to cater to the booming commercial nano and microsatellite launch market on an 'on-demand' basis. Features three solid propulsion stages and a terminal velocity correction module (TVCM).
| Vehicle Name | Payload Capacity (LEO / GTO) | Primary Application | |
|---|---|---|---|
| PSLV | Earth Observation / Remote Sensing | ||
| GSLV Mk II | Communication Satellites | ||
| LVM3 | Heavy Communication & Deep Space | ||
| SSLV | Small / Nano Satellites |