About: List of Thor-Able launches

An Entity of Type: rocket, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The Thor-Able (Thor DM-18-Able) was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960. It was a two-stage rocket, consisting of a Thor IRBM as a first stage and a Vanguard-derived Able second stage. On some flights, an Altair solid rocket motor was added as a third stage. It was a member of the Thor family and an early predecessor of the Delta.

Property	Value
dbo:MeanOfTransportation/diameter	2.44 (dbd:metre)
dbo:MeanOfTransportation/height	26900.0 (dbd:millimetre)
dbo:MeanOfTransportation/mass	51608.0 (dbd:kilogram)
dbo:Rocket/mass	51608.0 (dbd:kilogram)
dbo:abstract	The Thor-Able (Thor DM-18-Able) was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960. It was a two-stage rocket, consisting of a Thor IRBM as a first stage and a Vanguard-derived Able second stage. On some flights, an Altair solid rocket motor was added as a third stage. It was a member of the Thor family and an early predecessor of the Delta. (en)
dbo:comparable	dbr:Luna_(rocket)
dbo:diameter	2.440000 (xsd:double)
dbo:failedLaunches	6 (xsd:nonNegativeInteger)
dbo:finalFlight	1960-04-01 (xsd:date)
dbo:height	26.900000 (xsd:double)
dbo:launchSite	dbr:Cape_Canaveral_Air_Force_Station dbr:Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17
dbo:maidenFlight	1958-04-24 (xsd:date)
dbo:manufacturer	dbr:Aerojet dbr:Douglas_Aircraft_Company
dbo:mass	51608000.000000 (xsd:double)
dbo:rocketFunction	dbr:Sounding_rocket dbr:Expendable_launch_system
dbo:rocketStages	2 (xsd:nonNegativeInteger)
dbo:successfulLaunches	10 (xsd:nonNegativeInteger)
dbo:successor	dbr:Thor-Ablestar dbr:Delta_(rocket_family)
dbo:thumbnail	wiki-commons:Special:FilePath/Thor-Able_II_Transit_1A.jpg?width=300
dbo:totalLaunches	16 (xsd:nonNegativeInteger)
dbo:wikiPageExternalLink	https://space.skyrocket.de/doc_lau_det/thor-dm18_able.htm%7Caccess-date=2021-08-03%7Cwebsite=Gunter's
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dbp:caption	Launch of the Transit 1A satellite (en) on a Thor-Able II (en)
dbp:comparable	dbr:Luna_(rocket)
dbp:countryOrigin	United States (en)
dbp:derivatives	dbr:Thor-Ablestar dbr:Delta_(rocket_family)
dbp:fail	6 (xsd:integer)
dbp:family	dbr:Thor_(rocket_family)
dbp:first	1958-04-24 (xsd:date)
dbp:function	dbr:Sounding_rocket dbr:Expendable_launch_system
dbp:height	– (en)
dbp:last	1960-04-01 (xsd:date)
dbp:launches	16 (xsd:integer)
dbp:manufacturer	dbr:Aerojet dbr:Douglas_Aircraft_Company
dbp:payloads	dbr:Pioneer_program dbr:Transit_(satellite) dbr:Television_Infrared_Observation_Satellite
dbp:sites	dbr:Cape_Canaveral_Air_Force_Station dbr:Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17
dbp:stages	2 (xsd:integer)
dbp:success	10 (xsd:integer)
dbp:upright	1 (xsd:integer)
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dcterms:subject	dbc:Lists_of_rocket_launches dbc:Lists_of_Thor_and_Delta_launches dbc:Lists_of_Thor_launches
rdf:type	owl:Thing dbo:MeanOfTransportation wikidata:Q41291 dbo:Rocket
rdfs:comment	The Thor-Able (Thor DM-18-Able) was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960. It was a two-stage rocket, consisting of a Thor IRBM as a first stage and a Vanguard-derived Able second stage. On some flights, an Altair solid rocket motor was added as a third stage. It was a member of the Thor family and an early predecessor of the Delta. (en)
rdfs:label	List of Thor-Able launches (en)
owl:sameAs	wikidata:List of Thor-Able launches https://global.dbpedia.org/id/FyYZe
prov:wasDerivedFrom	wikipedia-en:List_of_Thor-Able_launches?oldid=1094194954&ns=0
foaf:depiction	wiki-commons:Special:FilePath/Thor-Able_II_Transit_1A.jpg
foaf:isPrimaryTopicOf	wikipedia-en:List_of_Thor-Able_launches
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