|
gptkbp:instanceOf
|
nuclear thermal rocket engine program
|
|
gptkbp:cancellationDate
|
1973
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:developedBy
|
gptkb:Atomic_Energy_Commission
gptkb:NASA
1955-1973
|
|
gptkbp:engineType
|
nuclear thermal rocket
|
|
gptkbp:fuelType
|
liquid hydrogen
|
|
gptkbp:fullName
|
gptkb:Nuclear_Engine_for_Rocket_Vehicle_Application
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NERVA
|
|
gptkbp:intendedUse
|
manned Mars missions
upper stage for Saturn V
|
|
gptkbp:legacy
|
influenced later nuclear propulsion concepts
|
|
gptkbp:locationOfArtifacts
|
gptkb:Smithsonian_National_Air_and_Space_Museum
|
|
gptkbp:notableFor
|
gptkb:NRX-A6
gptkb:NRX-EST
gptkb:XE_Prime
|
|
gptkbp:purpose
|
develop nuclear thermal rocket engines for space exploration
|
|
gptkbp:reactorType
|
solid-core nuclear reactor
|
|
gptkbp:relatedTo
|
gptkb:SNTP
gptkb:Project_Rover
|
|
gptkbp:specificImpulseVacuum
|
up to 850 seconds
|
|
gptkbp:status
|
cancelled
|
|
gptkbp:testedBy
|
gptkb:Nevada_Test_Site
|
|
gptkbp:thrust
|
up to 250,000 pounds-force
|
|
gptkbp:bfsParent
|
gptkb:Nuclear_Engine_for_Rocket_Vehicle_Application
gptkb:Project_Rover
|
|
gptkbp:bfsLayer
|
7
|