http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-106938965-B

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http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B21-0058
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06D5-06
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-06
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B21-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B31-28
filingDate 2016-10-13-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2018-08-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2018-08-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-106938965-B
titleOfInvention A kind of nitric acid ammonium low burn temperature clean fuel gas propellant
abstract A kind of nitric acid ammonium low burn temperature clean fuel gas propellant, including ammonium nitrate:65% ~ 80%, fire warm conditioning agent:0%~15%;Special additive:0% ~ 2%, adhesive:10% ~ 20%, curing agent:0.5% ~ 2.0%, other additives:2.0% ~ 6.0%, special additive is one kind or the combination of chrome green or vanadic anhydride, adhesive is terminal hydroxy group polyethylene oxide tetrahydrofuran, and curing agent is one kind or the combination of isophorone diisocyanate or toluene di-isocyanate(TDI) or modified six methine polyisocyanates.The gas generator propellant that the present invention produces, raw material are free of metal powder, have the characteristics that low burn temperature, combustion gas cleaning and non-corrosive gas, low residue and performance can easily be accommodated, the conventional weapon auxiliary power source that can be used for wide Acclimation temperature range, is especially applicable for the auxiliary power source for having particular/special requirement to combustion gas.
priorityDate 2016-10-13-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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