About: S400 (rocket engine)

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The S400 is a family of pressure fed liquid propelled rocket engines manufactured by ArianeGroup (former Airbus DS) at the Orbital Propulsion Centre in Lampoldshausen, Germany. They burn MMH and MON as propellant, have a thrust range between 340 newtons (76 lbf) and 450 newtons (100 lbf) and can vary the O/F ratio between 1.50 and 1.80. The chamber and throat are made of a platinum alloy, it uses double cone vortex injectors and uses both film and radiative cooling. The S400 engines are used as primary apogee engines for telecommunication satellite platforms such as the Spacebus of Thales Alenia Space as well as space exploration missions such as Venus Express, ExoMars Trace Gas Orbiter or Jupiter Icy Moons Explorer.

Attributes	Values
rdfs:label	S400 (rocket engine) (en)
rdfs:comment	The S400 is a family of pressure fed liquid propelled rocket engines manufactured by ArianeGroup (former Airbus DS) at the Orbital Propulsion Centre in Lampoldshausen, Germany. They burn MMH and MON as propellant, have a thrust range between 340 newtons (76 lbf) and 450 newtons (100 lbf) and can vary the O/F ratio between 1.50 and 1.80. The chamber and throat are made of a platinum alloy, it uses double cone vortex injectors and uses both film and radiative cooling. The S400 engines are used as primary apogee engines for telecommunication satellite platforms such as the Spacebus of Thales Alenia Space as well as space exploration missions such as Venus Express, ExoMars Trace Gas Orbiter or Jupiter Icy Moons Explorer. (en)
name	S400 (en)
dcterms:subject	Rocket engines using hypergolic propellant Rocket engines using the pressure-fed cycle
Wikipage page ID	46987629 (xsd:integer)
Wikipage revision ID	1068484476 (xsd:integer)
Link from a Wikipage to another Wikipage	Mixed oxides of nitrogen Alloy Venus Express Meteosat Platinum Pressure-fed engine Rocket engines using hypergolic propellant Rocket engines using the pressure-fed cycle Geostationary orbit Germany Monomethylhydrazine Orbital Propulsion Centre Communications satellite Syracuse (satellite) Liquid rocket propellant ARSAT-2 Hispasat AG1 ArianeGroup Jupiter Icy Moons Explorer Thales Alenia Space Spacebus ExoMars Trace Gas Orbiter Specific impulse Rocket propellant Symphonie Rocket engine Liquid Apogee Engine Rocket Engines Attitude dynamics and control Bipropellant rocket
sameAs	S400 (rocket engine) S400 (rocket engine) S400 (rocket engine) S400 (rocket engine)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Orbital_spacecraft_rocket_engines dbt:Reflist dbt:Rocket-stub
combustion chamber	1 (xsd:integer)
country of origin	Germany
cycle	Pressure-fed engine
designer	ArianeGroup
first date	1974-12-19 (xsd:date)
fuel	Monomethylhydrazine
mixture ratio	1.500000 (xsd:double)
oxidiser	Mixed oxides of nitrogen
purpose	Liquid Apogee Engine
status	Operational (en)
type	liquid (en)
used in	Communications satellite
has abstract	The S400 is a family of pressure fed liquid propelled rocket engines manufactured by ArianeGroup (former Airbus DS) at the Orbital Propulsion Centre in Lampoldshausen, Germany. They burn MMH and MON as propellant, have a thrust range between 340 newtons (76 lbf) and 450 newtons (100 lbf) and can vary the O/F ratio between 1.50 and 1.80. The chamber and throat are made of a platinum alloy, it uses double cone vortex injectors and uses both film and radiative cooling. The S400 engines are used as primary apogee engines for telecommunication satellite platforms such as the Spacebus of Thales Alenia Space as well as space exploration missions such as Venus Express, ExoMars Trace Gas Orbiter or Jupiter Icy Moons Explorer. The S400 family has had an extensive history on the commercial telecommunication market. Its first launch was aboard the Symphonie 1 in 1974. This was the first commercial three-axis stabilized communications satellite in geostationary orbit with a bipropellant rocket propulsion system. It also was the first European communications satellite system. This family of engines have displayed a remarkable competitiveness, still winning many designs (for 2015, it is expected to fly on Sicral 2, ARSAT-2, Hispasat AG1 and MSG-4. (en)
burn time	30600.0 (second)
gold:hypernym	Family
prov:wasDerivedFrom	wikipedia-en:S400_(rocket_engine)?oldid=1068484476&ns=0
page length (characters) of wiki page	4559 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:S400_(rocket_engine)
is Link from a Wikipage to another Wikipage of	DFS Kopernikus-3 EUTELSAT II F-1 Eutelsat 12 West B Eutelsat 21B Eutelsat 8 West B Eutelsat 8 West C Palapa-D Hispasat 1D Thaicom 5 S400
is foaf:primaryTopic of	wikipedia-en:S400_(rocket_engine)

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