SRM-2
E837379
SRM-2 is a solid-fuel rocket motor used as the second stage of the Inertial Upper Stage to propel payloads from low Earth orbit to higher or geosynchronous orbits.
Statements (25)
| Predicate | Object |
|---|---|
| instanceOf |
rocket stage
ⓘ
solid-fuel rocket motor ⓘ |
| associatedWith |
geosynchronous orbit
ⓘ
low Earth orbit ⓘ |
| controlMethod | thrust vector control (TVC) on upper stage ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| designedFor | high-energy orbital transfers ⓘ |
| ignitionSequence | ignited after completion of first stage burn ⓘ |
| launchContext | used after delivery of IUS and payload to low Earth orbit by a launch vehicle ⓘ |
| missionProfile | upper-stage transfer from parking orbit ⓘ |
| operationalEnvironment | space ⓘ |
| operator | United States space missions NERFINISHED ⓘ |
| partOf | two-stage Inertial Upper Stage system ⓘ |
| primaryFunction |
to propel payloads from low Earth orbit to geosynchronous orbit
ⓘ
to propel payloads from low Earth orbit to higher orbits ⓘ |
| propellantType | solid propellant ⓘ |
| propulsionType | solid rocket motor ⓘ |
| roleInMission | provides final velocity increment for payload deployment ⓘ |
| stageNumber | second stage ⓘ |
| thrustGenerationMethod | combustion of solid propellant grain ⓘ |
| usedFor |
orbit raising
ⓘ
transfer to geosynchronous orbit ⓘ |
| usedIn |
Inertial Upper Stage
NERFINISHED
ⓘ
satellite deployment missions to geosynchronous orbit ⓘ |
| usedWith | SRM-1 NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.