ASLV
E902164
ASLV (Augmented Satellite Launch Vehicle) was an early Indian small-lift launch vehicle developed by ISRO as a technological stepping stone toward more advanced rockets like the PSLV.
Statements (46)
| Predicate | Object |
|---|---|
| instanceOf |
expendable launch system
ⓘ
launch vehicle ⓘ small-lift launch vehicle ⓘ |
| abbreviationOf | Augmented Satellite Launch Vehicle NERFINISHED ⓘ |
| agencyProgram | Indian space program NERFINISHED ⓘ |
| configuration | solid-propellant launch vehicle ⓘ |
| countryOfOrigin | India ⓘ |
| developer | Indian Space Research Organisation NERFINISHED ⓘ |
| diameter | 1.0 m ⓘ |
| fairingType | payload shroud for small satellites ⓘ |
| firstFlightDate | 1987-03-24 ⓘ |
| firstLaunchOutcome | failure ⓘ |
| firstStageType | SLV-3 first stage with strap-on boosters ⓘ |
| fourthLaunchOutcome | success ⓘ |
| guidanceSystem | inertial guidance ⓘ |
| height | 23 m ⓘ |
| lastFlightDate | 1994-05-04 ⓘ |
| launchAzimuth | eastward from Sriharikota ⓘ |
| launchPad | SLP ⓘ |
| launchSite | Satish Dhawan Space Centre NERFINISHED ⓘ |
| launchVehicleFamily | SLV family ⓘ |
| liftOffMass | about 41 t ⓘ |
| manufacturer | Indian Space Research Organisation NERFINISHED ⓘ |
| notableMission | ASLV-D4 / SROSS-C2 NERFINISHED ⓘ |
| numberOfFailures | 2 ⓘ |
| numberOfLaunches | 4 ⓘ |
| numberOfPartialFailures | 1 GENERATED ⓘ |
| numberOfSuccessfulLaunches | 1 ⓘ |
| operatedBy | Indian Space Research Organisation NERFINISHED ⓘ |
| operatorAgency | Department of Space, Government of India NERFINISHED ⓘ |
| orbitType | low Earth orbit ⓘ |
| payloadToLEO | about 150 kg ⓘ |
| propulsionType | solid fuel ⓘ |
| purpose |
stepping stone to PSLV
ⓘ
technology demonstrator ⓘ |
| retirementReason | replaced by more capable PSLV ⓘ |
| secondLaunchOutcome | failure ⓘ |
| stages | 4 ⓘ |
| status | retired ⓘ |
| strapOnBoosters | 2 ⓘ |
| successor | PSLV NERFINISHED ⓘ |
| testbedFor |
staging techniques
ⓘ
vehicle dynamics and control for larger launchers ⓘ |
| thirdLaunchOutcome | partial failure ⓘ |
| usedFor |
development of multi-stage guidance and control
ⓘ
qualification of solid rocket motor technologies ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.