About: Intelsat III F-4

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Intelsat III F-4 was a geostationary communications satellite built by TRW, it was owned by Intelsat, a company currently based in Luxembourg. The satellite had an estimated useful life of 5 years. The Intelsat III F-4 was part of the Intelsat III series which consisted of eight satellites, which were used for retransmission of global commercial telecommunications, including live TV. The satellite was successfully launched into space on May 22, 1969, by means of a Delta M vehicle from Cape Canaveral Air Force Station in Florida, United States. It had a launch mass of 293 kg.

Attributes	Values
rdf:type	Thing schema:Event dul:Event societal event wikidata:Q1656682 wikidata:Q2133344 event space mission
rdfs:label	Intelsat III F-4 (en) Intelsat III F-4 (pt)
rdfs:comment	O Intelsat III F-4 era um satélite de comunicação geoestacionário construído pela TRW, ele era de propriedade da Intelsat, empresa atualmente sediada em Luxemburgo. O satélite tinha uma vida útil estimada de 5 anos. (pt) Intelsat III F-4 was a geostationary communications satellite built by TRW, it was owned by Intelsat, a company currently based in Luxembourg. The satellite had an estimated useful life of 5 years. The Intelsat III F-4 was part of the Intelsat III series which consisted of eight satellites, which were used for retransmission of global commercial telecommunications, including live TV. The satellite was successfully launched into space on May 22, 1969, by means of a Delta M vehicle from Cape Canaveral Air Force Station in Florida, United States. It had a launch mass of 293 kg. (en)
foaf:name	Intelsat III F-4 (en)
name	Intelsat III F-4 (en)
dcterms:subject	Spacecraft launched in 1969 Intelsat satellites
Wikipage page ID	53827727 (xsd:integer)
Wikipage revision ID	1009873942 (xsd:integer)
Link from a Wikipage to another Wikipage	Cape Canaveral Air Force Station United States Communications Geocentric orbit Geostationary orbit NASA Communication Delta M TRW Inc. Spacecraft launched in 1969 Florida Telecommunications Intelsat satellites Intelsat Intelsat III F-3 Intelsat III F-5 Satellite Geostationary Cape Canaveral Air Force Station Launch Complex 17 NiCd
sameAs	Intelsat III F-4 Intelsat III F-4 Intelsat III F-4 Intelsat III F-4
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_spaceflight dbt:Reflist dbt:Start-date dbt:Orbital_launches_in_1969 dbt:Intelsat
apsis	gee (en)
COSPAR ID	1969 (xsd:integer)
image caption	Intelsat III F-4. (en)
launch contractor	NASA
launch date	0001-05-22 (xsd:gMonthDay)
launch rocket	Delta M
launch site	Cape Canaveral Air Force Station Cape Canaveral Air Force Station Launch Complex 17
manufacturer	TRW Inc.
mission duration	1.57788E8 (second)
mission type	Communications
next mission	Intelsat III F-5
operator	Intelsat
orbit inclination	0.500000 (xsd:double)
orbit period	85134.0 (second)
orbit reference	Geocentric orbit
orbit regime	Geostationary orbit
previous mission	Intelsat III F-3
programme	Intelsat III (en)
SATCAT	3947 (xsd:integer)
has abstract	Intelsat III F-4 was a geostationary communications satellite built by TRW, it was owned by Intelsat, a company currently based in Luxembourg. The satellite had an estimated useful life of 5 years. The Intelsat III F-4 was part of the Intelsat III series which consisted of eight satellites, which were used for retransmission of global commercial telecommunications, including live TV. The satellite was stabilized by rotation with a minus antenna structure (its antenna was 34 inches high). It had a hydrazine propulsion system with four propellers and four tanks. Passive thermal control. With solar cells producing 178W peak, nine Ahr NiCd batteries. The load consisted of two transponders that used 12 watt TWTA amplifiers for multiple access, 1500 audio circuits or four TV channels. The Intelsat III F-1 was disabled due to launch vehicle failure. The satellite was successfully launched into space on May 22, 1969, by means of a Delta M vehicle from Cape Canaveral Air Force Station in Florida, United States. It had a launch mass of 293 kg. (en) O Intelsat III F-4 era um satélite de comunicação geoestacionário construído pela TRW, ele era de propriedade da Intelsat, empresa atualmente sediada em Luxemburgo. O satélite tinha uma vida útil estimada de 5 anos. (pt)
disposal type	Decommissioned (en)
orbit eccentricity	0.004710 (xsd:double)
orbit epoch	1969-05-22 (xsd:date)
prov:wasDerivedFrom	wikipedia-en:Intelsat_III_F-4?oldid=1009873942&ns=0
mission duration (μ)	1826.25 (day)
page length (characters) of wiki page	3510 (xsd:nonNegativeInteger)
COSPAR id	1969-045A
launch date	1969-05-22 (xsd:date)
mission duration (s)	157788000.000000 (xsd:double)
SATCAT	03947
launch vehicle	Delta M
manufacturer	TRW Inc.
next mission	Intelsat III F-5
operator	Intelsat
previous mission	Intelsat III F-3
type	Communications
foaf:isPrimaryTopicOf	wikipedia-en:Intelsat_III_F-4
is Link from a Wikipage to another Wikipage of	1969 in spaceflight List of Intelsat satellites Intelsat III F-3 Intelsat III F-5
is next mission of	Intelsat III F-3
is previous mission of	Intelsat III F-5
is next mission of	Intelsat III F-3
is previous mission of	Intelsat III F-5
is foaf:primaryTopic of	wikipedia-en:Intelsat_III_F-4

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