| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_856434bbf8bd6688fd565f65ca54e32c |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G7-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G7-00 |
| filingDate |
1967-06-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1971-03-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c9909da2c5facee063301da942779a7c |
| publicationDate |
1971-03-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3566670-A |
| titleOfInvention |
Reentry vehicle heat shield testing apparatus and method |
| abstract |
AN APPARATUS AND METHOD FOR TESTING REENTRY VEHICLE HEAT SHIELDS WHICH UTILIZES A HIGH PRESSURE HOT GAS GENERATOR WHICH OPERATES ON THE CHEMICAL-TO-THERMAL ENERGY CONVERSION PRINCIPLE WITH AN OXIDIZER-FUEL COMBINATION WHICH YIELDS COMBUSTION PRODUCTS SIMULATING HEAT SHIELD DEGRADATION PHENOMENA OF A SELECTED PLANETARY ATMOSPHERE. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9010178-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6146240-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2012192629-A1 |
| priorityDate |
1967-06-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |