http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-19756794-B4
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c2a2228cd30ede6827f8f6503e711daf |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06D5-00 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-00 |
filingDate | 1997-12-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 2005-10-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d26d902437ecdbfecca9667b8f64e3b8 |
publicationDate | 2005-10-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | DE-19756794-B4 |
titleOfInvention | Modular, cryogenic solid rocket propellant |
abstract | modular,ncryogenic solid rocket propellant with fuel assemblies of various typesnFuel components, such as fuels, oxidizers, energy-enhancingnAdditions,nBinder additives etc., for allnusualnand other applications of solid rocket, wherein the propellantnis at least partially fragmented, i. that at least onenthe component is not in the conventionalnintimate blend with the other components, but in the form of anor more macroscopic fuel bundles of any suitable purposengeometric design is present, characterized in thatnat least one of the fuel elements by the particular choice of hisnComposition is suitable, as a permanent Zündfackelgenerator or combustionnpromotionalnGas generator fornto serve the rest of the propellant. |
priorityDate | 1997-12-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 23.