Q3642311: Difference between revisions
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{{Page|booster separation motor|Classes|small rocket motors that separate a solid rocket booster from the main rocket body}} | {{Page|booster separation motor|Classes|small rocket motors that separate a solid rocket booster from the main rocket body|BSM}} | ||
Latest revision as of 15:59, 17 February 2025
The booster separation motors or BSMs on the Space Shuttle were relatively small rocket motors that separated the reusable solid rocket boosters (SRB) from the orbiter after SRB burnout. Eight booster separation motors were attached to each of the shuttle's two reusable solid rocket boosters, four on the forward frustum and four on the aft skirt.
Wikidata
BSM
mass 75.75 kilogram, mass 41.3 kilogram, length 790 millimetre, diameter 327 millimetre,
Northrop Grumman,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, solid propellant rocket engine, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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