This HTML5 document contains 100 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/
n11http://dbpedia.org/resource/File:
n13https://global.dbpedia.org/id/
schemahttp://schema.org/
dbthttp://dbpedia.org/resource/Template:
rdfshttp://www.w3.org/2000/01/rdf-schema#
n14http://www.ontologydesignpatterns.org/ont/dul/DUL.owl#
n9http://commons.wikimedia.org/wiki/Special:FilePath/
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/

Statements

Subject Item
dbr:OV1-86
rdf:type
wikidata:Q1656682 dbo:SocietalEvent dbo:SpaceMission dbo:Event owl:Thing n14:Event wikidata:Q2133344 schema:Event
rdfs:label
OV1-86
rdfs:comment
Orbiting Vehicle 1-86 (also known as OV1-86 ) was a satellite launched 27 July 1967 to measure the temperature radiation properties of different types of terrain. Part of the OV1 series of USAF satellites, using standardized designs and sent to orbit on decommissioned Atlas ICBMs to reduce development and launching costs, OV1-86 was launched with two other satellites in the series, OV1-11 and OV1-12, in the first triple launch of the program. It was the only OV1 satellite to be cobbled together from two of its sister satellites, utilizing the unused body on OV1-8 and the unused propulsion module on OV1-6. OV1-86's was only partially successful due to the failure of its Vertistat gravity-gradient_stabilization system. The satellite reentered the Earth's atmosphere on 22 February 1972.
foaf:name
OV1-86
dbp:name
OV1-86
foaf:depiction
n9:OV1-86.jpg n9:OV1-86_launch.jpg n9:OV1-86_oxygen_radiometer.jpg
dcterms:subject
dbc:Spacecraft_launched_in_1967 dbc:Spacecraft_which_reentered_in_1972 dbc:Military_satellites
dbo:wikiPageID
71359794
dbo:wikiPageRevisionID
1112318265
dbo:wikiPageWikiLink
dbr:OV1-5 dbr:OV1-6 dbr:OV1-7 dbr:OV1-8 dbr:Vandenberg_Air_Force_Base_Launch_Complex_576 dbr:Cosmic_ray_telescope dbr:Watt dbc:Spacecraft_launched_in_1967 dbr:Earth_science dbr:USAF dbr:Isotropy n11:OV1-86_launch.jpg dbr:Altair_(rocket_stage) n11:OV1-86_oxygen_radiometer.jpg dbr:Eastern_Range dbr:OPS_0855 dbr:Atlas_D dbr:ICBM dbr:OV1-13 dbr:Gravity-gradient_stabilization dbr:Orbiting_Vehicle dbr:Low_Earth_Orbit dbc:Spacecraft_which_reentered_in_1972 dbr:Western_Range_(USSF) dbr:Dicke_radiometer dbr:General_Dynamics dbr:Kelvin dbr:Hertz dbr:OV1-1 dbc:Military_satellites dbr:SM-65_Atlas dbr:OV1-11 dbr:OV1-12 dbr:High_test_peroxide dbr:Titan_IIIC
owl:sameAs
n13:GRHun wikidata:Q111854289
dbp:wikiPageUsesTemplate
dbt:Convert dbt:Infobox_spaceflight dbt:Start-date dbt:Short_description dbt:Reflist dbt:Rp dbt:Orbital_launches_in_1967
dbo:thumbnail
n9:OV1-86.jpg?width=300
dbp:apsis
gee
dbp:cosparId
1967
dbp:decayDate
1972-02-22
dbp:imageCaption
OV1-86 on a cart awaiting installation on its Atlas rocket
dbp:imageSize
180
dbp:launchDate
0001-07-27
dbp:launchRocket
dbr:Atlas_D
dbp:launchSite
dbr:Vandenberg_Air_Force_Base_Launch_Complex_576
dbp:manufacturer
dbr:General_Dynamics
dbp:missionType
dbr:Earth_science
dbp:nextMission
dbr:OV1-13
dbp:operator
dbr:USAF
dbp:orbitInclination
101.6
dbp:orbitPeriod
5730.0
dbp:orbitRegime
dbr:Low_Earth_Orbit
dbp:previousMission
dbr:OV1-12
dbp:programme
OV1
dbp:satcat
S02893
dbo:abstract
Orbiting Vehicle 1-86 (also known as OV1-86 ) was a satellite launched 27 July 1967 to measure the temperature radiation properties of different types of terrain. Part of the OV1 series of USAF satellites, using standardized designs and sent to orbit on decommissioned Atlas ICBMs to reduce development and launching costs, OV1-86 was launched with two other satellites in the series, OV1-11 and OV1-12, in the first triple launch of the program. It was the only OV1 satellite to be cobbled together from two of its sister satellites, utilizing the unused body on OV1-8 and the unused propulsion module on OV1-6. OV1-86's was only partially successful due to the failure of its Vertistat gravity-gradient_stabilization system. The satellite reentered the Earth's atmosphere on 22 February 1972.
dbp:launchMass
with Altair
dbp:orbitEccentricity
0.00895
dbp:orbitEpoch
0001-07-27
prov:wasDerivedFrom
wikipedia-en:OV1-86?oldid=1112318265&ns=0
dbo:wikiPageLength
10685
dbo:cosparId
1967-072A
dbo:landingDate
1972-02-22
dbo:launchDate
1967-07-27
dbo:satcat
S02893
dbo:launchVehicle
dbr:Atlas_D
dbo:manufacturer
dbr:General_Dynamics
dbo:nextMission
dbr:OV1-13
dbo:operator
dbr:USAF
dbo:previousMission
dbr:OV1-12
dbo:type
dbr:Earth_science
foaf:isPrimaryTopicOf
wikipedia-en:OV1-86