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.
Attributes | Values |
---|
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
| |
dcterms:subject
| |
Wikipage page ID
| |
Wikipage revision ID
| |
Link from a Wikipage to another Wikipage
| |
sameAs
| |
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
| |
fuel
| |
length
| |
manufacturer
| |
oxidiser
| |
status
| |
type
| |
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)
|
gold:hypernym
| |
prov:wasDerivedFrom
| |
page length (characters) of wiki page
| |
foaf:isPrimaryTopicOf
| |
is Link from a Wikipage to another Wikipage
of | |
is successor
of | |
is foaf:primaryTopic
of | |