Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine
|
| gptkbp:animationStudio |
±8_degrees
|
| gptkbp:controls |
digital
fly-by-wire redundant systems |
| gptkbp:coolingSystem |
regenerative cooling
|
| gptkbp:design |
F-1 engine
|
| gptkbp:developer |
$1 billion
|
| gptkbp:dosageForm |
1,500 pounds per second
|
| gptkbp:engine |
2011
training programs advanced materials public demonstrations computer models international partnerships modular ongoing studies 14.5 feet controlled awards and honors static fire test two igniters detailed engineering data space exploration advancements coolant channels influence on new technologies |
| gptkbp:engineDisplacement |
7.5 feet
real-time monitoring technical manuals |
| gptkbp:engineType |
periodic inspections
high reliability staged combustion |
| gptkbp:fireDepartment |
1,000 psi
|
| gptkbp:firstFlight |
1981
2011 |
| gptkbp:fuel_capacity |
1,000 pounds per second
|
| gptkbp:fuelType |
liquid hydrogen and liquid oxygen
hypergolic |
| gptkbp:hasArea |
gptkb:NASA_Stennis_Space_Center
|
| gptkbp:hasContent |
452 seconds
|
| gptkbp:hasDepartment |
8.5 minutes
|
| https://www.w3.org/2000/01/rdf-schema#label |
Space Shuttle main engines
|
| gptkbp:manufacturer |
Rocketdyne
|
| gptkbp:numberOfEpisodes |
three
|
| gptkbp:operatingHours |
closed cycle
|
| gptkbp:operationalHistory |
part_of_Space_Shuttle_program
|
| gptkbp:operationalStatus |
3,000 °F
3,000 psi |
| gptkbp:performances |
influenced future designs
|
| gptkbp:propulsion |
yes
1,000,000 pounds 143:1 |
| gptkbp:reliability |
yes
|
| gptkbp:totalGoals |
135 engines
|
| gptkbp:usedIn |
Space Shuttle
|
| gptkbp:weight |
7,000 pounds
|