|
abbreviation
|
GSLV Mk III / LVM3
self-linksurface differs
ⓘ
surface form:
Geosynchronous Satellite Launch Vehicle Mark III
|
|
agencyProgramme
|
Indian human spaceflight programme
ⓘ
|
|
alsoKnownAs
|
LVM3
ⓘ
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commercialLaunchProvider
|
NewSpace India Limited
ⓘ
|
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configuration
|
three-stage launch vehicle
ⓘ
|
|
countryOfOrigin
|
India
ⓘ
|
|
designedFor
|
crewed spacecraft launch capability
ⓘ
|
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developmentAgency
|
Liquid Propulsion Systems Centre
ⓘ
|
|
developmentAgency
|
Vikram Sarabhai Space Centre
ⓘ
|
|
fairingDiameter
|
about 5 metres
ⓘ
|
|
family
|
Geosynchronous Satellite Launch Vehicle
ⓘ
surface form:
GSLV launch vehicle family
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|
firstFlight
|
18 December 2014
ⓘ
|
|
firstFlightType
|
suborbital test flight
ⓘ
|
|
firstOrbitalFlight
|
5 June 2017
ⓘ
|
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firstOrbitalMission
|
GSAT-19
ⓘ
|
|
firstStageDesignation
|
S200
ⓘ
|
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firstStageType
|
solid rocket motor
ⓘ
|
|
gtoPayloadCapacity
|
about 4 tonnes
ⓘ
|
|
height
|
about 43 metres
ⓘ
|
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instanceOf
|
expendable launch system
ⓘ
|
|
instanceOf
|
heavy-lift launch vehicle
ⓘ
|
|
instanceOf
|
orbital launch vehicle
ⓘ
|
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launchAzimuthRange
|
equatorial to geosynchronous orbits
ⓘ
|
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launchPad
|
Second Launch Pad, Satish Dhawan Space Centre
ⓘ
|
|
launchSite
|
Satish Dhawan Space Centre
ⓘ
|
|
launchedPayload
|
OneWeb satellites
ⓘ
|
|
leoPayloadCapacity
|
about 8 tonnes
ⓘ
|
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liftOffMass
|
about 640 tonnes
ⓘ
|
|
manufacturer
|
Indian Space Research Organisation
ⓘ
|
|
marketedAs
|
LVM3 for commercial launches
ⓘ
|
|
notableMission
|
Chandrayaan-2
ⓘ
|
|
notableMission
|
Chandrayaan-3
ⓘ
|
|
notableMission
|
Gaganyaan test missions
ⓘ
|
|
operator
|
Indian Space Research Organisation
ⓘ
|
|
primaryRole
|
launching communication satellites to geostationary transfer orbit
ⓘ
|
|
propulsionType
|
solid, liquid, and cryogenic stages
ⓘ
|
|
reliabilityRecord
|
multiple successful orbital missions
ⓘ
|
|
secondStageDesignation
|
L110
ⓘ
|
|
secondStagePropellant
|
UH25 and nitrogen tetroxide
ⓘ
|
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secondStageType
|
liquid engine stage
ⓘ
|
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secondaryRole
|
supporting crewed space missions
ⓘ
|
|
status
|
operational
ⓘ
|
|
strapOnBoosters
|
two S200 solid rocket boosters
ⓘ
|
|
successorTo
|
GSLV Mk II for heavier payloads
ⓘ
|
|
thirdStageDesignation
|
C25
ⓘ
|
|
thirdStageEngine
|
CE-20 cryogenic engine
ⓘ
|
|
thirdStagePropellant
|
liquid oxygen and liquid hydrogen
ⓘ
|
|
thirdStageType
|
cryogenic upper stage
ⓘ
|
|
usedFor
|
GSLV Mk III / LVM3
self-linksurface differs
ⓘ
surface form:
ISRO Gaganyaan programme
|