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.

All labels observed (1)

Label Occurrences
SRM-2 canonical 2

How this entity was disambiguated

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 ⓘ
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 ⓘ
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 ⓘ
satellite deployment missions to geosynchronous orbit ⓘ
usedWith SRM-1 ⓘ

How these facts were elicited

Referenced by (2)

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