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- Star_37 abstract "The Star 37 is a type of solid rocket motor used by many space propulsion and launch vehicle stages. It is used almost exclusively as an upper stage. It was developed primarily by Thiokol Propulsion, and now manufactured by ATK (now Orbital ATK) who purchased Thiokol corporation.The Star 37 was first used as the engine for the Thor-Burner upper stage. The Burner I used the Thiokol FW-4 (TE 364-1) engine and the Burner 2 used the Thiokol (TE-M-364-2).The "-37" designation refers to the approximate diameter of the fuel casing in inches; Thiokol had also manufactured other motors such as the Star-40 and Star 48. Internally, Thiokol's designation was TE-M-364 for early versions, TE-M-714 for later ones, and TE-M-783 for a special HTPB model used for FLTSATCOM launches.Subtypes are given one or more letter suffixes after the diameter number, or a trailing number (i.e., "-2") after the internal designation. Not surprisingly, the "T" prefix stands for Thiokol, and the following letter refers to the company division that developed the rocket motor. In this case, "M" refers to the Magna, UT Division. "E" refers to the Elkton, MD division.The Star 37FM rocket motor was developed and qualified for use as an apogee kick motor on FLTSATCOM. The motor is a replacement for the Star 37E Delta, which has been discontinued. The Nozzle assembly uses a 3D carbon-carbon throat and a carbon-phenolic exit cone. Maximum propellant weight is 2350 pounds, while the motor has been qualified for propellant off-loading to 2257 pounds. The Star 37XFP rocket motor has been qualified as the orbit insertion motor for Rockwell International's (now Boeing) Global Positioning Satellite (GPS), and as the apogee motor for the RCA SATCOM Ku-Band satellite. The Star 37XFP motor can be used as a replacement for the Star 37F motor, which has been discontinued.".
- Star_37 wikiPageExternalLink star-37.htm.
- Star_37 wikiPageID "36037037".
- Star_37 wikiPageLength "8174".
- Star_37 wikiPageOutDegree "26".
- Star_37 wikiPageRevisionID "673320840".
- Star_37 wikiPageWikiLink Alliant_Techsystems.
- Star_37 wikiPageWikiLink Atlas_(rocket_family).
- Star_37 wikiPageWikiLink Burner_(rocket_stage).
- Star_37 wikiPageWikiLink Category:Alliant_Techsystems.
- Star_37 wikiPageWikiLink Category:Rocket_engines.
- Star_37 wikiPageWikiLink Category:Rocket_stages.
- Star_37 wikiPageWikiLink Category:Solid-fuel_rockets.
- Star_37 wikiPageWikiLink Delta_(rocket_family).
- Star_37 wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
- Star_37 wikiPageWikiLink Launch_vehicle.
- Star_37 wikiPageWikiLink Multistage_rocket.
- Star_37 wikiPageWikiLink Orbital_ATK.
- Star_37 wikiPageWikiLink Solid-fuel_rocket.
- Star_37 wikiPageWikiLink Solid_rocket.
- Star_37 wikiPageWikiLink Spacecraft.
- Star_37 wikiPageWikiLink Staging_(rocketry).
- Star_37 wikiPageWikiLink Star_27.
- Star_37 wikiPageWikiLink Star_48.
- Star_37 wikiPageWikiLink Thiokol.
- Star_37 wikiPageWikiLink Thor-Burner.
- Star_37 wikiPageWikiLink Thor_(rocket_family).
- Star_37 wikiPageWikiLink Titan_(rocket_family).
- Star_37 wikiPageWikiLink USA.
- Star_37 wikiPageWikiLink United_States.
- Star_37 wikiPageWikiLinkText "Star 37".
- Star_37 wikiPageWikiLinkText "Star 37D".
- Star_37 wikiPageWikiLinkText "Star 37E".
- Star_37 wikiPageWikiLinkText "Star 37FM".
- Star_37 wikiPageWikiLinkText "Star-37".
- Star_37 wikiPageWikiLinkText "Star-37D".
- Star_37 wikiPageWikiLinkText "Star-37E".
- Star_37 wikiPageWikiLinkText "Star-37S-ISS".
- Star_37 combustionChamber "1".
- Star_37 countryOfOrigin USA.
- Star_37 countryOfOrigin United_States.
- Star_37 date "1963".
- Star_37 diameter "0.66 m".
- Star_37 dryWeight "113.0".
- Star_37 hasPhotoCollection Star_37.
- Star_37 length "2.27 m".
- Star_37 name "Star-37".
- Star_37 predecessor Star_27.
- Star_37 purpose "Upper stage/Spacecraft propulsion".
- Star_37 status "Active".
- Star_37 successor Star_48.
- Star_37 thrust(vac)_ "33.600 kN".
- Star_37 type "solid".
- Star_37 usedIn "Thor (rocket family), Delta (rocket family), upper stage".
- Star_37 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Star_37 wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- Star_37 wikiPageUsesTemplate Template:Reflist.
- Star_37 wikiPageUsesTemplate Template:Rocket_Engines.
- Star_37 wikiPageUsesTemplate Template:Upper_stages.
- Star_37 subject Category:Alliant_Techsystems.
- Star_37 subject Category:Rocket_engines.
- Star_37 subject Category:Rocket_stages.
- Star_37 subject Category:Solid-fuel_rockets.
- Star_37 hypernym Motor.
- Star_37 type Person.
- Star_37 type Stage.
- Star_37 comment "The Star 37 is a type of solid rocket motor used by many space propulsion and launch vehicle stages. It is used almost exclusively as an upper stage. It was developed primarily by Thiokol Propulsion, and now manufactured by ATK (now Orbital ATK) who purchased Thiokol corporation.The Star 37 was first used as the engine for the Thor-Burner upper stage.".
- Star_37 label "Star 37".
- Star_37 sameAs Star_37.
- Star_37 sameAs m.0j_3hw5.
- Star_37 sameAs Q15977211.
- Star_37 sameAs Q15977211.
- Star_37 wasDerivedFrom Star_37?oldid=673320840.
- Star_37 isPrimaryTopicOf Star_37.