http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-H0640792-A
Outgoing Links
Predicate | Object |
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assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_ba54aff29064e18f1e36be0d4d17be67 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-02 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B23-007 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B23-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-02 |
filingDate | 1993-01-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d945677c6e1042cf816f98a186797f49 |
publicationDate | 1994-02-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | JP-H0640792-A |
titleOfInvention | Rocket engine propellant composition |
abstract | (57) [Summary] [Purpose] To provide a rocket engine propellant composition. A solid rocket engine propellant composition capable of burning at least two specific burning velocities is provided. The burning rate is controlled by controlling the pressure at which the propellant burns. For example, it is possible to change the container in which the propellant is held, for example a rocket engine casing, in order to change the pressure on combustion of the propellant. Alternatively, the propellant may be shaped or shaped such that the pressure changes at a particular time due to the combustion process of the propellant. The propellant can burn at a relatively constant burn rate at a specific pressure. If the pressure changes within a certain limit, the burning rate of the propellant quickly changes to another relatively constant burning rate. The solid rocket engine propellant is manufactured with the addition of about 0.5 to about 4.0% TiO 2 . The specific operating pressure and the burning rate can be selected by changing the amount of TiO 2 added, the particle sizes of various components and the specific components used. |
isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2012531380-A |
priorityDate | 1992-01-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 38.