Properties (64)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
launch vehicle
|
| gptkbp:developedBy |
gptkb:Indian_Space_Research_Organisation
|
| gptkbp:firstFlight |
September 20, 1993
|
| gptkbp:fuelType |
solid and liquid
|
| gptkbp:hasPartnershipsWith |
2001
|
| gptkbp:height |
44 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
PSLV
|
| gptkbp:internationalCooperation |
yes
|
| gptkbp:launched |
multiple launches per year
|
| gptkbp:launchSite |
gptkb:Satish_Dhawan_Space_Centre
|
| gptkbp:notableFeature |
cost-effective
Chandrayaan-1 Mars Orbiter Mission has undergone several upgrades versatile design PSLV-C37 high payload flexibility first Indian rocket to launch a satellite into a polar orbit capable of launching multiple satellites first Indian rocket to reach Mars has a command and control system has a launch escape system has a launch vehicle assembly system has a launch vehicle environmental control system has a launch vehicle ground support system has a launch vehicle integration system has a launch vehicle maintenance system has a launch vehicle mission analysis system has a launch vehicle mission documentation system has a launch vehicle mission evaluation system has a launch vehicle mission execution system has a launch vehicle mission feedback system has a launch vehicle mission improvement system has a launch vehicle mission planning system has a launch vehicle mission reporting system has a launch vehicle mission review system has a launch vehicle mission simulation system has a launch vehicle mission training system has a launch vehicle operation system has a launch vehicle quality assurance system has a launch vehicle recovery system has a launch vehicle refurbishment system has a launch vehicle safety system has a launch vehicle testing system has a launch vehicle transportation system has a modular design has a payload fairing has a proven track record has a telemetry system has a tracking system has been operational for over 30 years used for launching foreign satellites uses a combination of solid and liquid propulsion used_for_launching_Indian_satellites |
| gptkbp:number_of_stages |
4 stages
|
| gptkbp:payloadCapacity |
up to 3,800 kg to GTO
|
| gptkbp:reliability |
high
|
| gptkbp:setting |
gptkb:PSLV-QL
PSLV-XL PSLV-CA PSLV-DL |
| gptkbp:succeededBy |
over 90%
|
| gptkbp:usedFor |
satellite launches
|
| gptkbp:weight |
320 tons
|