Kosmos-3M

E400700

Kosmos-3M was a Soviet and later Russian two-stage orbital launch vehicle widely used from the 1960s to the 2000s to place small satellites into low Earth orbit.

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All labels observed (2)

Label Occurrences
Cosmos-3M 1
Kosmos-3M canonical 1

Statements (47)

Predicate Object
instanceOf expendable launch system
orbital launch vehicle
alsoKnownAs Kosmos-3M
surface form: Cosmos-3M
countryOfOrigin Russia
Soviet Union
derivedFrom R-14 Chusovaya missile
surface form: R-14 missile
diameter about 2.4 meters
family Kosmos rocket family
firstFlightDate 1967-11-16
firstStageEngineType RD-219
firstStageRole initial ascent and boost phase
fuelType nitrogen tetroxide / UDMH
guidanceSystem inertial guidance
intendedOrbit low Earth orbit
launchAzimuthRange various inclinations from Plesetsk
launchConfiguration two-stage liquid-fueled rocket
two-stage stacked configuration
launchMass about 109000 kilograms
launchRecord one of the most frequently flown Soviet/Russian launchers
launchSitesUsed Kapustin Yar
Plesetsk Cosmodrome
length about 32 meters
manufacturer PO Polyot
Yuzhnoye Design Bureau
notableUse launch of communications satellites
launch of military satellites
launch of scientific satellites
numberOfStages 2
operatedBy Russian Aerospace Forces
surface form: Russian Space Forces

Soviet space program
surface form: Soviet Space Program
operatorType military
originTechnology ballistic missile conversion
payloadToLEO approximately 1400 kilograms
programPeriod Cold War era
propellantType liquid
retirementDate 2010-04-27
role orbital insertion of small payloads
secondStageEngineType RD-219
surface form: RD-219M
serviceLife over 40 years
status retired
successor Rokot
successRate high
totalLaunches over 440
typicalPayloadClass small satellites
upperStageRole final orbit insertion
usedFromDecade 1960s
usedUntilDecade 2010s

Referenced by (2)

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

Kosmos-3M alsoKnownAs Kosmos-3M
this entity surface form: Cosmos-3M