http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10914559-B1

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http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B15-01
filingDate 2018-09-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2021-02-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fea4e9116556e33e17c8f2022a556d10
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publicationDate 2021-02-09-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-10914559-B1
titleOfInvention Missile, slot thrust attitude controller system, and method
abstract The embodiments disclosed include a system comprising a missile segment having a hollow body with an external surface conforming to an external surface of a portion of a missile body. The missile segment comprises a plurality of slot thrust motor (STM) cavities arranged in the hollow body. Each STM cavity being elongated in a first direction relative to a longitudinal axis of the missile body. Each STM cavity includes a chamfered opening at one end of the STM cavity coincident with the external surface of the hollow body. The chamfered opening configured to expel a stream of a gas in a gas-flow direction which is at least one of perpendicular to and offset from the longitudinal axis. The embodiments also include a missile and method for producing a steering force.
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