Jupiter Engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instanceOf engine
gptkbp:application launch vehicles
gptkbp:chemicalFormula cryogenic
gptkbp:collaborations international space agencies
with universities
gptkbp:component lightweight alloys
gptkbp:controls digital
gptkbp:coolingSystem regenerative cooling
gptkbp:culturalImpact inspired films and literature
gptkbp:design 20 missions
applied in design
gptkbp:designedFor gptkb:spacecraft
gptkbp:developedBy NASA
gptkbp:documentType bell nozzle
gptkbp:education STEM programs
gptkbp:energyEfficiency high
gptkbp:environmentalImpact low emissions
gptkbp:fireDepartment around 1,000 psi
gptkbp:firstFlight 1990
gptkbp:fuelType cryogenic
hypergolic
gptkbp:future_plans next-generation engines
gptkbp:futurePlans deep space missions
gptkbp:hasArea gptkb:Marshall_Space_Flight_Center
gptkbp:hasDepartment about 500 seconds
https://www.w3.org/2000/01/rdf-schema#label Jupiter Engine
gptkbp:inspiration future propulsion technologies
gptkbp:integration modular design
gptkbp:launched cost-effective
gptkbp:launchSite gptkb:Kennedy_Space_Center
gptkbp:legacy significant in aerospace history
gptkbp:maintenance minimal
gptkbp:mediaCoverage extensive
gptkbp:operationalStatus active
extreme
gptkbp:patentCitation numerous innovations
gptkbp:performance high thrust-to-weight ratio
gptkbp:produces over 100,000 pounds
gptkbp:productionCompany 1980
gptkbp:propulsion yes
high
gptkbp:publicAccess widely recognized
showcased at events
gptkbp:related_engine staged combustion
gptkbp:reliability proven
gptkbp:researchAndDevelopment ongoing
gptkbp:safetyFeatures redundant systems
gptkbp:successor gptkb:J-2X_Engine
gptkbp:technology overcome during development
gptkbp:usedBy liquid oxygen
gptkbp:usedIn Space Shuttle
gptkbp:uses liquid hydrogen
gptkbp:weight approximately 3,000 pounds