This HTML5 document contains 59 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
dctermshttp://purl.org/dc/terms/
dbohttp://dbpedia.org/ontology/
foafhttp://xmlns.com/foaf/0.1/
n16https://global.dbpedia.org/id/
n12http://dbpedia.org/resource/Template:Infobox_rocket/
yagohttp://dbpedia.org/class/yago/
dbthttp://dbpedia.org/resource/Template:
rdfshttp://www.w3.org/2000/01/rdf-schema#
freebasehttp://rdf.freebase.com/ns/
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
owlhttp://www.w3.org/2002/07/owl#
wikipedia-enhttp://en.wikipedia.org/wiki/
dbphttp://dbpedia.org/property/
dbchttp://dbpedia.org/resource/Category:
provhttp://www.w3.org/ns/prov#
xsdhhttp://www.w3.org/2001/XMLSchema#
wikidatahttp://www.wikidata.org/entity/
dbrhttp://dbpedia.org/resource/
n17https://web.archive.org/web/20161228023324/http:/astronautix.com/s/

Statements

Subject Item
dbr:Saturn_V-B
rdf:type
owl:Thing wikidata:Q41291 dbo:Rocket yago:Vehicle104524313 yago:PhysicalEntity100001930 yago:Conveyance103100490 yago:Whole100003553 yago:Instrumentality103575240 yago:Object100002684 yago:Artifact100021939 yago:Rocket104099429 dbo:MeanOfTransportation
rdfs:label
Saturn V-B
rdfs:comment
Studied in 1968 by Marshall Space Flight Center, the Saturn V-B was considered an interesting vehicle concept because it nearly represents a single-stage to orbit booster, but is actually a stage and a half booster just like the Atlas. The booster would achieve liftoff via five regular F-1 engines; four of the five engines on the Saturn V-B would be jettisoned and could be fully recoverable, with the sustainer stage on the rocket continuing the flight into orbit. The rocket could have had a good launch capability similar to that of the Space Shuttle if it was constructed, but it never flew.
foaf:name
Saturn V-B
dbp:name
Saturn V-B
dcterms:subject
dbc:Saturn_(rocket_family)
dbo:wikiPageID
11097780
dbo:wikiPageRevisionID
1104762248
dbo:wikiPageWikiLink
dbr:Space_Shuttle dbr:Single-stage_to_orbit dbr:Moon dbr:Rocketdyne dbr:Saturn-Shuttle dbc:Saturn_(rocket_family) dbr:RP-1 dbr:Launch_vehicle dbr:F-1_(rocket_engine) dbr:Stage_and_a_half dbr:Low_Earth_orbit dbr:Atlas_(missile) dbr:LOX dbr:Marshall_Space_Flight_Center
dbo:wikiPageExternalLink
n17:saturnv-b.html
owl:sameAs
freebase:m.02q_yd_ wikidata:Q7426805 n16:4uWW8
dbp:sites
Unknown
dbp:wikiPageUsesTemplate
dbt:Rocketry-stub n12:payload dbt:Saturns dbt:Infobox_rocket dbt:Unreferenced dbt:Cvt n12:stage
dbp:status
Concept/study
dbp:stages
1.5
dbo:abstract
Studied in 1968 by Marshall Space Flight Center, the Saturn V-B was considered an interesting vehicle concept because it nearly represents a single-stage to orbit booster, but is actually a stage and a half booster just like the Atlas. The booster would achieve liftoff via five regular F-1 engines; four of the five engines on the Saturn V-B would be jettisoned and could be fully recoverable, with the sustainer stage on the rocket continuing the flight into orbit. The rocket could have had a good launch capability similar to that of the Space Shuttle if it was constructed, but it never flew.
dbp:countryOrigin
United States
dbp:function
Crewed/uncrewed LEO and Lunar launch vehicle
dbp:launches
0
dbo:rocketFunction
dbr:Low_Earth_orbit dbr:Moon
prov:wasDerivedFrom
wikipedia-en:Saturn_V-B?oldid=1104762248&ns=0
dbo:wikiPageLength
1817
dbo:status
Concept/study
dbo:totalLaunches
0
dbo:rocketStages
2
foaf:isPrimaryTopicOf
wikipedia-en:Saturn_V-B