http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-203113-U1
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64G1-22 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-22 |
| filingDate | 2020-07-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2021-03-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2021-03-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | RU-203113-U1 |
| titleOfInvention | BINARY SPACE WITH RECONFIGURABLE SCANNING ANTENNA COMBINED WITH A SOLAR BATTERY DEPLOYABLE MULTIVECTOR MATRIX ROCKET ENGINES |
| abstract | The utility model relates to small binary spacecraft (BSC) designed to create reconfigurable scanning multi-element antenna systems. The spacecraft contains two cylindrical bodies, in the centers of the ends of which there are three telescopic rods, on which there are three multi-vector matrix rocket engines (MMRD) with wavy cylindrical surfaces for deploying a flexible solar battery (SB) coiled in two rolls, integrated with an antenna. Cloth SB consists of two parts of equal length, the ends of which are connected to cylindrical bodies and to tension tubes, in which retractable docking manipulators are located. The rotation of one web relative to the other is carried out by an electromechanical unit consisting of a coaxially located annular solar sensor, a disk current collector, a stepper motor connecting the first and second tension tubes in the middle. To control the long deployment of the SB and the orientation of the SC relative to the other SCs with the help of the MMRD, four disk scanning laser rangefinders, mounted on the ends of the cylindrical bodies, are used. The technical result is the possibility of docking with several SC, the deployment and folding of the SB, integrated with the antenna, directly coiled or wound onto the cylindrical housings using the MMRD, their compact parking at the end of the SC collapse and the possibility of simultaneous separate tracking of the SB for the Sun and moving in different directions sources of radio signals. |
| priorityDate | 2020-07-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.