Solid Rocket Booster
E175569
The Solid Rocket Booster is a large, reusable solid-fuel rocket used to provide the majority of thrust during the initial phase of a space shuttle’s ascent.
All labels observed (4)
| Label | Occurrences |
|---|---|
| Space Shuttle Solid Rocket Booster | 2 |
| Solid Rocket Booster canonical | 1 |
| Space Shuttle Solid Rocket Booster program | 1 |
| Space Shuttle solid rocket boosters | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T1523464 — resolving that mention is where its identity was fixed. The disambiguator weighed these candidate entities and picked the highlighted one (or “None”, minting a new entity). This is how homonymy is resolved: the same surface form can point to different entities.
Target entity: Solid Rocket Booster Context triple: [Space Transportation System, component, Solid Rocket Booster]
-
A.
Redstone rocket
The Redstone rocket was an early American ballistic missile adapted by NASA as a reliable launch vehicle for the first crewed Mercury spaceflights.
-
B.
Interim Cryogenic Propulsion Stage
The Interim Cryogenic Propulsion Stage is a liquid hydrogen–liquid oxygen upper stage used on early NASA Space Launch System missions to provide orbital insertion and translunar injection capability before the introduction of a more powerful exploration upper stage.
-
C.
Super Heavy booster
The Super Heavy booster is SpaceX’s massive first-stage rocket designed to provide the primary lift for the fully reusable Starship launch system.
-
D.
LC-39B
LC-39B is a launch pad at NASA’s Kennedy Space Center that has supported major crewed and uncrewed space missions, including Space Shuttle flights and later Space Launch System operations.
-
E.
LC-39A
LC-39A is a historic launch pad at NASA’s Kennedy Space Center in Florida, used for Apollo Moon missions, Space Shuttle flights, and later commercial launches including SpaceX Falcon rockets.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
Target entity: Solid Rocket Booster Target entity description: The Solid Rocket Booster is a large, reusable solid-fuel rocket used to provide the majority of thrust during the initial phase of a space shuttle’s ascent.
-
A.
Redstone rocket
The Redstone rocket was an early American ballistic missile adapted by NASA as a reliable launch vehicle for the first crewed Mercury spaceflights.
-
B.
Interim Cryogenic Propulsion Stage
The Interim Cryogenic Propulsion Stage is a liquid hydrogen–liquid oxygen upper stage used on early NASA Space Launch System missions to provide orbital insertion and translunar injection capability before the introduction of a more powerful exploration upper stage.
-
C.
Super Heavy booster
The Super Heavy booster is SpaceX’s massive first-stage rocket designed to provide the primary lift for the fully reusable Starship launch system.
-
D.
LC-39B
LC-39B is a launch pad at NASA’s Kennedy Space Center that has supported major crewed and uncrewed space missions, including Space Shuttle flights and later Space Launch System operations.
-
E.
LC-39A
LC-39A is a historic launch pad at NASA’s Kennedy Space Center in Florida, used for Apollo Moon missions, Space Shuttle flights, and later commercial launches including SpaceX Falcon rockets.
- F. None of above. chosen
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
solid-fuel rocket booster
ⓘ
space shuttle component ⓘ |
| abbreviation | SRB ⓘ |
| attachedTo | Space Shuttle Orbiter via External Tank ⓘ |
| burnTime | approximately 124 seconds ⓘ |
| componentOf |
Space Shuttle launch stack
ⓘ
linked to:
Space Shuttle stack
|
| contains | segments of solid propellant ⓘ |
| countryOfOrigin |
United States
ⓘ
linked to:
United States of America
|
| designFeature | segment joints with field joints ⓘ |
| developedFor |
Space Shuttle program
ⓘ
linked to:
NASA Space Shuttle program
|
| failureCauseInChallenger | O-ring failure in field joint ⓘ |
| failureInvolvedIn | Space Shuttle Challenger disaster ⓘ |
| guidance | thrust vector control system ⓘ |
| ignition | simultaneous at liftoff with Space Shuttle Main Engines ⓘ |
| influencedDesignOf |
Space Launch System solid rocket boosters
ⓘ
linked to:
SLS solid rocket boosters
|
| isReusable | true ⓘ |
| laterManufacturer |
ATK Launch Systems
ⓘ
Northrop Grumman Innovation Systems ⓘ
linked to:
Northrop Grumman
|
| launchPad |
Launch Complex 39A
ⓘ
linked to:
Kennedy Space Center Launch Complex 39A
Launch Complex 39B ⓘ
linked to:
Kennedy Space Center Launch Complex 39B
|
| launchSite | Kennedy Space Center ⓘ |
| manufacturer |
Morton Thiokol
ⓘ
Thiokol ⓘ |
| massContribution | major portion of total launch thrust ⓘ |
| material | steel case ⓘ |
| mountedOn | sides of the Space Shuttle External Tank ⓘ |
| numberPerLaunch | 2 ⓘ |
| operatedBy | NASA ⓘ |
| postFlightProcessing | refurbishment and refilling with propellant ⓘ |
| propellantType | solid propellant ⓘ |
| provides | majority of thrust during initial ascent ⓘ |
| recoveredBy | parachute descent into the ocean ⓘ |
| recoveryFeature |
nose cap with parachute system
ⓘ
separation motors ⓘ |
| recoveryMethod | ocean splashdown and retrieval by ship ⓘ |
| role | augment main engine thrust during ascent ⓘ |
| safetyImprovement | redesigned field joints after Challenger ⓘ |
| separatesAt | approximately two minutes after liftoff ⓘ |
| shutdownCapability | no in-flight shutdown ⓘ |
| thrustAtLiftoff | approximately 12.5 MN each ⓘ |
| usedByAgency |
NASA Space Shuttle Program
ⓘ
linked to:
NASA Space Shuttle program
|
| usedFor | launch vehicle first-stage thrust ⓘ |
| usedFrom | 1981 ⓘ |
| usedInProgram | Space Transportation System ⓘ |
| usedOn | Space Shuttle ⓘ |
| usedOnMission |
STS-1
ⓘ
STS-135 ⓘ |
| usedUntil | 2011 ⓘ |
How these facts were elicited
The pipeline generated the facts above by prompting gpt-5.1 with this entity's name + description and the instruction below.
You are a knowledge base construction expert. Given a subject entity and a description of it, return factual statements that you know for the subject as a JSON list of dictionaries(triples), where keys must be "subject", "predicate" and "object". The number of facts may be very high, between 25 to 50 or more, for very popular subjects. For less popular subjects, the number of facts can be very low, like 5 or 10. # Requirements - If you don't know the subject at all, return an empty list. - If the subject is not a named entity, return an empty list. - Include at least one triple where predicate is "instanceOf". - Do not get too wordy. - Separate several objects into multiple triples with one object.
Subject: Solid Rocket Booster Description of subject: The Solid Rocket Booster is a large, reusable solid-fuel rocket used to provide the majority of thrust during the initial phase of a space shuttle’s ascent.
Referenced by (5)
Full triples — surface form annotated when it differs from this entity's canonical label.