Solid rocket boosters for Space Shuttle
GPTKB entity
Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:assemblyLocation |
gptkb:Kennedy_Space_Center
|
| gptkbp:burnTime |
about 2 minutes
|
| gptkbp:component |
casing
nozzle forward skirt aft skirt propellant segments |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.71 meters
|
| gptkbp:emptyWeight |
91,000 kg
|
| gptkbp:failureCauseInChallenger |
O-ring erosion
|
| gptkbp:firstFlight |
gptkb:STS-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Solid rocket boosters for Space Shuttle
|
| gptkbp:lastFlight |
gptkb:STS-135
|
| gptkbp:length |
45.46 meters
|
| gptkbp:manufacturer |
gptkb:Thiokol
|
| gptkbp:massLoaded |
590,000 kg
|
| gptkbp:numberOfLaunches |
2
|
| gptkbp:propulsion |
ammonium perchlorate composite propellant
|
| gptkbp:recoveryMethod |
parachute and ocean splashdown
|
| gptkbp:reusable |
true
|
| gptkbp:separationAltitude |
45 km
|
| gptkbp:thrust |
12.5 MN
|
| gptkbp:usedInDisaster |
gptkb:Challenger_disaster
|
| gptkbp:usedOn |
gptkb:Space_Shuttle
|
| gptkbp:bfsParent |
gptkb:ATK_Launch_Systems
|
| gptkbp:bfsLayer |
6
|