PSLV-CA

E259990

PSLV-CA is a variant of India’s Polar Satellite Launch Vehicle designed for launching smaller payloads into orbit using a configuration without solid strap-on boosters.

All labels observed (1)

Label Occurrences
PSLV-CA canonical 7

How this entity was disambiguated

Statements (46)

Predicate Object
instanceOf expendable launch system ⓘ
launch vehicle variant ⓘ
orbital launch vehicle ⓘ
abbreviationOf Polar Satellite Launch Vehicle ⓘ
surface form: Polar Satellite Launch Vehicle – Core Alone
agency Indian Space Research Organisation ⓘ
surface form: ISRO
belongsToProgram Indian civilian space program ⓘ
configurationFeature core-alone configuration without solid strap-on boosters ⓘ
countryOfOrigin India ⓘ
designedForOrbitType low Earth orbit ⓘ
polar orbit ⓘ
sun-synchronous orbit ⓘ
designGoal cost-effective access to polar and sun-synchronous orbits for small payloads ⓘ
developedIn India ⓘ
familyIncludesVariant PSLV-G ⓘ
PSLV-XL ⓘ
familyVariantOf PSLV launch vehicle family ⓘ
surface form: PSLV
firstStageType solid rocket motor ⓘ
fourthStageType liquid rocket engine ⓘ
guidanceType inertial navigation system ⓘ
launchAzimuth primarily polar and sun-synchronous trajectories ⓘ
launchCapability launching smaller payloads to orbit ⓘ
launchEnvironment expendable, single-use per mission ⓘ
launchHistory used in multiple ISRO missions ⓘ
launchPadUsed First Launch Pad, Satish Dhawan Space Centre ⓘ
Second Launch Pad, Satish Dhawan Space Centre ⓘ
launchSite Satish Dhawan Space Centre ⓘ
launchVehicleRole satellite deployment ⓘ
manufacturer Indian Space Research Organisation ⓘ
missionType uncrewed ⓘ
notableFeature optimized for lighter payload missions ⓘ
simplified configuration compared to PSLV standard variants with strap-ons ⓘ
operator Indian Space Research Organisation ⓘ
partOfFamily Polar Satellite Launch Vehicle ⓘ
payloadType Earth observation satellites ⓘ
remote sensing satellites ⓘ
small scientific satellites ⓘ
propellantFirstStage HTPB-based solid propellant ⓘ
propellantFourthStage MMH and MON-3 ⓘ
propellantSecondStage UH25 and nitrogen tetroxide ⓘ
propellantThirdStage HTPB-based solid propellant ⓘ
secondStageType liquid rocket engine ⓘ
stageCount 4 ⓘ
status operational ⓘ
technologyType multistage chemical rocket ⓘ
thirdStageType solid rocket motor ⓘ
usedBy Indian Space Research Organisation ⓘ

How these facts were elicited

Referenced by (7)

Full triples — surface form annotated when it differs from this entity's canonical label.

NEOSSat → launchVehicle → PSLV-CA ⓘ
PSLV launch complex → supportsLaunchVehicle → PSLV-CA ⓘ
subject surface form: PSLV Launch Complex
Sapphire (satellite) → launchVehicle → PSLV-CA ⓘ
subject surface form: Sapphire
STRaND-1 → launchVehicle → PSLV-CA ⓘ
PSLV-G → successorVariant → PSLV-CA ⓘ