http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-3141354-C2
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-68 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-64 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-64 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-68 |
| filingDate | 1981-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 1986-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 1986-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | DE-3141354-C2 |
| titleOfInvention | Engine, in particular control engine for spacecraft |
| abstract | An engine, which is particularly suitable for the control of spacecraft, consists essentially of a decomposition chamber for the decomposition of predominantly liquid energy sources, which can be supplied with liquid fuel via an injection pipe, and an expansion nozzle for the propellant gases that is connected downstream of the decomposition chamber. Between the injection tube and the head part of the decomposition chamber facing it, a tubular adapter is provided, the inner diameter of which is greater than that of the injection tube and which encompasses the mouth area of the injection tube. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-4418536-C1 |
| priorityDate | 1981-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.