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filingDate 1994-10-20^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_33cee25ddf1a15c90338381bf5df3611
publicationDate 1996-04-25^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber DE-4437524-A1
titleOfInvention Method for operating a missile propulsion system and missile propulsion
abstract The description concerns a process for operating a reaction-type missile propulsion system and a propulsion system for implementing the process. The propulsion system is operated by causing silicon hydride compounds to react with nitrogen and/or nitrogen compounds at high temperatures in the presence of an oxidising agent for the hydrogen of the silicon hydride compounds. The nitrogen and the oxidising agent can be preferably taken from the earth's atmosphere, thus avoiding having to carry the oxidising agent for the silicon hydride compounds in the missile. The silicon hydride compounds burned are preferably silanols.
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