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RS-56 was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse.

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rdf:type
rdfs:label
  • RS-56 (motor cohete) (es)
  • RS-56 (en)
rdfs:comment
  • RS-56 era un motor cohete de combustible líquido americano, desarrollado por Rocketdyne. RS-56 se derivó del motor cohete RS-27. Se construyeron dos variantes de este motor, ambos para su uso en la serie de cohetes Atlas II.​ El primero, RS-56-OBA, era un motor de refuerzo,​ mientras que el RS-56-OSA se diseñó para usarse como sustentador y producir un empuje más bajo pero a un impulso específico más alto.​ (es)
  • RS-56 was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse. (en)
name
  • RS-56 (en)
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Wikipage revision ID
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specific impulse sea level
  • RS-56-OBA: (en)
  • RS-56-OSA: (en)
specific impulse vacuum
  • RS-56-OBA: (en)
  • RS-56-OSA: (en)
dbp:thrust(sl)_
  • RS-56-OBA: (en)
  • RS-56-OSA: (en)
dbp:wikiPageUsesTemplate
first flight
country of origin
cycle
diameter
  • RS-56-OBA: (en)
fuel
length
  • RS-56-OBA: (en)
manufacturer
oxidiser
status
  • retired (en)
type
  • liquid (en)
used in
has abstract
  • RS-56 era un motor cohete de combustible líquido americano, desarrollado por Rocketdyne. RS-56 se derivó del motor cohete RS-27. Se construyeron dos variantes de este motor, ambos para su uso en la serie de cohetes Atlas II.​ El primero, RS-56-OBA, era un motor de refuerzo,​ mientras que el RS-56-OSA se diseñó para usarse como sustentador y producir un empuje más bajo pero a un impulso específico más alto.​ (es)
  • RS-56 was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series. The first, RS-56-OBA, was a booster engine, while the RS-56-OSA was designed for use as a sustainer and produced lower thrust but at a higher specific impulse. (en)
burn time
  • 283.0 (second)
  • RS-56-OBA: 172 (en)
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page length (characters) of wiki page
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is Link from a Wikipage to another Wikipage of
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is foaf:primaryTopic of
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