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The Rocketdyne RS-2200 was an experimental linear aerospike rocket engine developed by Rocketdyne for Lockheed Martin's VentureStar program. The program was ultimately cancelled in 2001 before any RS-2200 engines were assembled.

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rdfs:label
  • RS-2200 (en)
rdfs:comment
  • The Rocketdyne RS-2200 was an experimental linear aerospike rocket engine developed by Rocketdyne for Lockheed Martin's VentureStar program. The program was ultimately cancelled in 2001 before any RS-2200 engines were assembled. (en)
name
  • RS-2200 (en)
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
sameAs
specific impulse sea level
specific impulse vacuum
thrust to weight
dbp:wikiPageUsesTemplate
country of origin
  • United States (en)
cycle
  • Gas-generator (en)
date
designer
  • Rocketdyne (en)
dimensions
  • Forward End: wide, long Aft End: wide, long Forward to Aft: (en)
fuel
  • LH2 (en)
mixture ratio
purpose
  • X-33 (en)
status
  • Development Canceled (en)
type
  • Liquid (en)
has abstract
  • The Rocketdyne RS-2200 was an experimental linear aerospike rocket engine developed by Rocketdyne for Lockheed Martin's VentureStar program. The program was ultimately cancelled in 2001 before any RS-2200 engines were assembled. (en)
associated
  • XRS-2200 (en)
nozzle
  • Linear Aerospike (en)
nozzle ratio
oxidizer
  • LOX (en)
prov:wasDerivedFrom
page length (characters) of wiki page
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is Link from a Wikipage to another Wikipage of
is foaf:primaryTopic of
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