ISRO has envisaged a number of variants of PSLV to cater to different mission requirements. There are currently three operational versions of the PSLV — the standard (PSLV), the core-alone (PSLV-CA) without the six strap-on booster motors, and the (PSLV-XL) version, which carries more solid fuel in its strap-on motors than the standard version. All the three versions have proved to be unalloyed successes.[3] These configurations provide wide variations in payload capabilities ranging from 600 kg in LEO to 1900 kg in sun synchronous orbit.
Variants
PSLV (Operational)
The standard version of the PSLV has four stages using solid and liquid propulsion systems alternately and six strap-on boosters. It currently has capability to launch 1,678 kg to 622 km into sun synchronous orbit.
PSLV-CA (Operational)
The PSLV-CA, CA meaning "Core Alone", model premiered on April 23, 2007. The CA model does not include the six strap-on boosters used by the PSLV standard variant. Two small roll control modules and two first stage motor control injection tanks were still attached to the side of the first stage.[4] The fourth stage of the CA variant has 400 kg less propellant when compared to its standard version.[4] It currently has capability to launch 1,100 kg to 622 km sun synchronous orbit.[5]
PSLV-XL (Operational)
PSLV-XL is the uprated version of Polar Satellite Launch Vehicle in its standard