| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_ab395b2c07eaab518bd911f5c01461da
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_97e3975f7695a1886a98c003bc668431
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_e68a57d9f4e6d1fb406dcd85ade059e3 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-64 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F28D15-00 |
| filingDate |
2006-08-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cf210a7c5e504e47cd499eed8dac7978
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_aeede42e0f6361dcc93723620df138ac
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b239128cc505c07959abe5d4b46c5a29 |
| publicationDate |
2010-09-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2010218482-A1 |
| titleOfInvention |
System and method for cooling rocket engines |
| abstract |
A propulsion system for a rocket engine and a method of cooling a rocket engine includes a propellant tank fluidically coupled to the rocket engine to hold a pressurized propellant, a coolant tank to hold a coolant, a first heat exchanger thermally coupled to the rocket engine and fluidically coupled to the coolant tank, a second heat exchanger thermally coupled to the propellant tank and fluidically coupled to the first heat exchanger, and a third heat exchanger disposed inside the propellant tank to thermally couple a propellant withdrawn from the tank for combustion to a propellant disposed inside the tank. The coolant flows from the coolant tank to the first heat exchanger and through the first heat exchanger to cool the rocket engine. The propellant withdrawn from the propellant tank receives heat from the propellant disposed inside the tank through the third heat exchanger to convert to a gaseous propellant when withdrawn from the propellant tank as a liquid propellant. The coolant flows from the first heat exchanger to the second heat exchanger and through the second heat exchanger to heat the propellant disposed inside the propellant tank. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10605203-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2514570-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2012131903-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016505765-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9222439-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9222438-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016510378-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016505764-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3786074-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11371468-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2012144797-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102019123057-A1 |
| priorityDate |
2006-08-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |