http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2142898-C1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_494b46ae73851c8179d79850b72b35d8 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-002 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-403 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B15-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-40 |
| filingDate | 1998-10-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 1999-12-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2124a209e15ff8015c4d4d819ac3d246 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_eeaa3169c171a6d223cd8f07690c7336 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ecb71f425b30a7a32ab9fe69332f636c http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3239649c2ff7a23c78fe5d23e90bd37d http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3c72dfeaba9472788bb73853a059d4e0 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ed16f9abeb0958ac5a137499591403f1 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f2dec9ec9fd37449c09e0ef38ada4048 |
| publicationDate | 1999-12-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | RU-2142898-C1 |
| titleOfInvention | Method for conversion of combat solid-propellant rockets into solid-propellant space rocket and space rocket |
| abstract | FIELD: space equipment, in particular, launch vehicles for injection of spacecraft to the near-earth orbit. SUBSTANCE: a four-stage space rocket is created on the basis of the stages of disassembled three- stage solid-propellant combat rockets (on expiration of their guaranteed service life). The first module of the space rocket has three sustainer stages of the first combat rocket, and the second module - one sustainer stage of the second combat rocket. The space rocket is furnished with a development (final) stage and a newly developed connecting module. Connected to the latter is the head unit from the spacecraft under the cone. At disassembly of combat rockets, for assembly and launching of space rocket from a spacecraft use is made of (modified) transport-launching packs of combat rockets. EFFECT: enhanced technical and economical efficiency, confirmed by successful launchings of the four-stage launch vehicle "Start 1". 31 cl, 11 dwg |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2619611-C1 |
| priorityDate | 1998-10-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 33.