SRM-1
E837378
SRM-1 is a solid rocket motor used as the first-stage propulsion unit for the Inertial Upper Stage space launch system.
Statements (25)
| Predicate | Object |
|---|---|
| instanceOf |
rocket engine
ⓘ
solid rocket motor ⓘ |
| application |
civilian satellite deployment
ⓘ
military satellite deployment ⓘ |
| configuration | two-stage Inertial Upper Stage system ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| developedFor |
NASA missions
ⓘ
U.S. Department of Defense missions ⓘ |
| ignitionSequence | ignited after deployment from primary launch vehicle ⓘ |
| missionProfile | boost payload from low Earth orbit to higher energy orbits ⓘ |
| operatedIn | Earth orbit missions ⓘ |
| partOf | Inertial Upper Stage NERFINISHED ⓘ |
| propellantType | solid propellant ⓘ |
| propulsionSystemType | single-use solid rocket motor ⓘ |
| role | boost phase propulsion ⓘ |
| stageNumber | first stage ⓘ |
| successorStage | SRM-2 NERFINISHED ⓘ |
| thrustType | vacuum-optimized solid rocket thrust ⓘ |
| usedAs | first-stage propulsion unit ⓘ |
| usedFor |
orbital transfer
ⓘ
space launch ⓘ |
| usedIn | Inertial Upper Stage space launch system NERFINISHED ⓘ |
| usedInProgram | Inertial Upper Stage program NERFINISHED ⓘ |
| usedWith |
Space Shuttle
NERFINISHED
ⓘ
Titan launch vehicles NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.