S-310 sounding rocket

E442450

The S-310 is a Japanese single-stage solid-fuel sounding rocket used primarily for upper-atmosphere and microgravity research missions.

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Label Occurrences
S-310 sounding rocket canonical 1

Statements (44)

Predicate Object
instanceOf solid-fuel rocket
sounding rocket
apogeeRange 100 to 200 kilometers
countryOfOrigin Japan
designedFor microgravity experiments
middle and upper atmosphere observations
developedIn Japan NERFINISHED
diameter 0.31 meters
firstFlight 1975
fuelType solid propellant
guidanceType unguided spin-stabilized
launchMass approximately 700 kilograms
launchOrganization Japan Aerospace Exploration Agency NERFINISHED
launchProfile vertical launch
launchSitesUsed Andøya Space Center NERFINISHED
Esrange Space Center NERFINISHED
Uchinoura Space Center NERFINISHED
length approximately 7.6 meters
manufacturer Institute of Space and Astronautical Science NERFINISHED
Japan Aerospace Exploration Agency NERFINISHED
missionEnvironment near-space
upper atmosphere
missionType suborbital
numberOfStages 1
operator Institute of Space and Astronautical Science NERFINISHED
Japan Aerospace Exploration Agency NERFINISHED
payloadType scientific instruments
predecessor K-9M sounding rocket NERFINISHED
primaryUse microgravity research
upper-atmosphere research
propulsionType solid rocket motor
recovery payload recovery by parachute
stabilizationMethod spin stabilization
stageConfiguration single-stage
status operational
successor S-520 sounding rocket NERFINISHED
typicalApogee approximately 150 kilometers
typicalFlightDuration several minutes
usedBy Japanese research institutions
international research collaborations
usedFor aeronomy studies
atmospheric composition measurements
microgravity material science experiments
plasma physics experiments

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Uchinoura Space Center launchesFromHere S-310 sounding rocket