About: Ascent propulsion system

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Rocket engine used by the Apollo Lunar Module

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Property Value
dbo:description
  • rocket engine used by the Apollo Lunar Module (en)
dbo:thumbnail
dbo:wikiPageExternalLink
dbo:wikiPageWikiLink
dbp:burnTime
  • 200.0 (dbd:second)
dbp:caption
  • Apollo LM ascent engine (en)
dbp:combustionChamber
  • 1 (xsd:integer)
dbp:countryOfOrigin
dbp:cycle
dbp:date
  • 1964 (xsd:integer)
dbp:fuel
dbp:manufacturer
dbp:mixtureRatio
  • 1.600000 (xsd:double)
dbp:name
  • Ascent propulsion system (en)
dbp:nozzleRatio
  • 46 (xsd:integer)
dbp:oxidiser
dbp:predecessor
  • Bell 8247 (en)
dbp:pumps
  • None (en)
dbp:purpose
  • Lunar Ascent Stage/Spacecraft propulsion (en)
dbp:restarts
  • Designed for 1 restarts (en)
dbp:status
  • Retired (en)
dbp:successor
dbp:thrustToWeight
  • 16.700000 (xsd:double)
dbp:type
  • liquid (en)
dbp:usedIn
  • Lunar module as ascent engine (en)
dbp:wikiPageUsesTemplate
dct:subject
rdfs:label
  • Ascent propulsion system (en)
  • Ascent Propulsion System (in)
  • 月着陸船用上昇エンジン (ja)
  • Ascent Propulsion System (pt)
owl:sameAs
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foaf:isPrimaryTopicOf
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