| Index: > A B C D E F G H I J K L M N O P Q R S T U V W X Y Z |
|
|||||
The vehicle consists of two solid-propellant stages (stage 1 and 3) and two liquid stages (2 and 4).
After some delays, the first launch of the PSLV occurred on 20 September 1993. Although all main engines performed as expected, an altitude control problem was reported in the second and third stages. After this initial setback, ISRO met success with the third developmental launch in 1996. Further successful launches followed in 1997, 1999, and 2001.
In September 2002, the 1060 kg KALPANA-1 was launched by PSLV-C4 to a GTO orbit (Geo Transfer Orbit). On 17 October 2003, the 1360kg Earth observingEarth observation satellites are satellites specifically designed to observe Earth from orbit, similar to reconnaissance satellites but intended for non-military uses such as environmental monitoring, meteorology, map making etc. Satellites or satellite s ResourceSat1 was launched by PSLV-C5.