patent/CA-2378019-A1

Predicate	Object
assignee	http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_e71ceee88045962115ff1db837e14116
classificationCPCInventive	http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-97
classificationIPCInventive	http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-97
filingDate	2000-07-03-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor	http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_fa581ed1747eb0c535399c3d0669ffe3
publicationDate	2001-01-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber	CA-2378019-A1
titleOfInvention	Erosion resistant rocket nozzle
abstract	A rocket nozzle having an inlet (10), a middle region (20), a throat (30) and an outlet, wherein a ratio of the cross-sectional area of the inlet to the throat is about 1.1. The middle region preferably has a shape which rises to an apex. Such a configuration places particles resulting from combustion on a trajectory which misses the wall of the nozzle at the throat or choke point, thereby decreasing throat erosion/ablation.
priorityDate	1999-07-02-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type	http://data.epo.org/linked-data/def/patent/Publication

Predicate	Subject
isDiscussedBy	http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID5480431 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419559581 http://rdf.ncbi.nlm.nih.gov/pubchem/taxonomy/TAXID4270 http://rdf.ncbi.nlm.nih.gov/pubchem/anatomy/ANATOMYID4270 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID297 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419506174

Total number of triples: 17.