S-520 sounding rocket
E443387
The S-520 is a Japanese single-stage solid-fuel sounding rocket used for suborbital scientific experiments and atmospheric research.
Statements (41)
| Predicate | Object |
|---|---|
| instanceOf |
sounding rocket
ⓘ
suborbital launch vehicle ⓘ |
| abbreviation | S-520 NERFINISHED ⓘ |
| category | Japanese sounding rocket ⓘ |
| countryOfOrigin | Japan ⓘ |
| crewCapacity | 0 ⓘ |
| developedIn | Japan NERFINISHED ⓘ |
| flightType | uncrewed ⓘ |
| fuelType | solid propellant ⓘ |
| launchCapability | sounding rocket missions ⓘ |
| launchEnvironment | upper atmosphere ⓘ |
| launchesFrom | Uchinoura Space Center NERFINISHED ⓘ |
| launchSite | Uchinoura Space Center NERFINISHED ⓘ |
| launchSiteCountry | Japan NERFINISHED ⓘ |
| launchTrajectory | suborbital trajectory ⓘ |
| manufacturer |
Institute of Space and Astronautical Science
NERFINISHED
ⓘ
Japan Aerospace Exploration Agency NERFINISHED ⓘ |
| missionProfile | suborbital flight ⓘ |
| missionType |
scientific research
ⓘ
technology demonstration ⓘ |
| numberOfStages | 1 ⓘ |
| operatedBy |
ISAS
NERFINISHED
ⓘ
JAXA NERFINISHED ⓘ |
| operator |
Institute of Space and Astronautical Science
NERFINISHED
ⓘ
Japan Aerospace Exploration Agency NERFINISHED ⓘ |
| payloadType | scientific instruments ⓘ |
| primaryUse |
atmospheric research
ⓘ
suborbital scientific experiments ⓘ |
| propellantType | solid ⓘ |
| propulsionStageCount | 1 ⓘ |
| propulsionType | solid-fuel rocket ⓘ |
| researchField |
atmospheric physics
ⓘ
plasma physics ⓘ space science ⓘ |
| stageConfiguration | single-stage ⓘ |
| status | operational ⓘ |
| usedBy |
Japanese scientific community
ⓘ
international research teams ⓘ |
| usedFor |
aeronomy studies
ⓘ
microgravity experiments ⓘ space science experiments ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.