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The Star is a family of US solid-propellant rocket motors originally developed by Thiokol and used by many space propulsion and launch vehicle stages. They are used almost exclusively as an upper stage, often as an apogee kick motor. Three Star 37 stages, and one Star 48 stage, were launched on solar escape trajectories; fast enough to leave the Sun's orbit and out into interstellar space, where barring the low chance of colliding with debris, they will travel past other stars in the Milky Way galaxy and survive potentially intact for millions of years.

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rdfs:label
  • Star (rakettrap) (nl)
  • Star (rocket stage) (en)
rdfs:comment
  • The Star is a family of US solid-propellant rocket motors originally developed by Thiokol and used by many space propulsion and launch vehicle stages. They are used almost exclusively as an upper stage, often as an apogee kick motor. Three Star 37 stages, and one Star 48 stage, were launched on solar escape trajectories; fast enough to leave the Sun's orbit and out into interstellar space, where barring the low chance of colliding with debris, they will travel past other stars in the Milky Way galaxy and survive potentially intact for millions of years. (en)
  • De Star is een Amerikaanse lijn van op vaste brandstof werkende raketmotoren en rakettrappen die als zogenaamde “kick-stage” aan draagraketten kunnen worden toegevoegd. De productie was door overnames en bedrijfsfusies achtereenvolgens in handen van Thiokol (tot 2001), Alliant Techsystems (2001-2015), Orbital ATK (2015-2018) en Northrop Grumman Innovation Systems (2018-2020) en Northrop Grumman Space Systems (sinds 2020). (nl)
name
  • Star 27 (en)
  • Star 48 (en)
  • Star-37 (en)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/PAM-D_rocket_stage.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Star-27.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/TE-M-364_Rocket_Engine_USAF.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
specific impulse vacuum
  • (en)
dbp:wikiPageUsesTemplate
thumbnail
caption
  • A Star-27 kick motor with nozzle for IBEX (en)
  • Star-48B rocket motor (en)
  • TE-M-364 (en)
combustion chamber
country of origin
  • United States (en)
date
diameter
  • 0.66 m (en)
image size
length
  • 2.27 m (en)
manufacturer
predecessor
purpose
  • Upper stage/Spacecraft propulsion (en)
status
  • Active (en)
successor
dbp:thrust(vac)_
  • 33.600 kN (en)
type
  • solid (en)
url
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