| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1cdff4e1c7e556bccfddfc162ca1fc05 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T29-49346 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-34 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B23P11-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-00 |
| filingDate |
2007-07-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_41ff98b7b2b1e297adc42963c4e98337 |
| publicationDate |
2010-02-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2010024428-A1 |
| titleOfInvention |
Rocket Apparatus and/or Method |
| abstract |
A rocket motor for one or more of limited re-use or single use, including a rocket motor housing, the motor housing adapted to contain propellant; an aft closure with a nozzle, the aft closure connected or connectable to the housing; a forward closure connected or connectable to the housing; wherein one or both of the aft closure and the forward closure are connectable to the housing in manner adapted for one or both of limited re-use or single use. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9416753-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2016356589-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10662898-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2014230678-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10066918-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10690467-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018106218-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10746133-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018073466-A1 |
| priorityDate |
2006-07-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |