Electric decoupling of the cathode gas feed line of the plasma accelerator
protected by the RF Patent
¹ 2298247
(application ¹ 2005135480 dated 16.11.2005)has been developed.
The patent is published in
the bulletin "Inventions. Utility models" ¹12, 2007.
Prime multi-chamber propulsion system with nozzle extension (variants)
protected by the RF Patent
¹ 2267026
(application ¹ 2005104257 dated 17.02.2005)has been developed.
The patent is published in
the bulletin "Inventions. Utility models" ¹36, 2005.
A method for determining maximum size of a membrane by the bubble method
is developed; it is protected by the RF patent
¹ 2248552
(application ¹ 2003115928 dated 29.05.2003).
The patent is published in
the bulletin "Inventions. Utility models" ¹8, 2005.
Droplet cooler-radiator was developed;
it is protected by the RF patent
¹ 2247064
(application ¹
2003121089 dated 14.07.2003).
The patent is published in
the bulletin "Inventions. Utility models" ¹2, 2005.
The installation for liquid filtration has been developed;
it is protected by the RF patent
¹ 2243022
(application ¹
2003116173 dated 03.06.2003).
The patent is published in
the bulletin "Inventions. Utility models" ¹36, 2004.
The injector assembly of the LRE chamber,protected by the RF patent
¹ 2225947
(application ¹
2002116120 dated 21.06.2002),has been developed.
The patent is published in
the bulletin "Inventions. Utility models",¹ 8, 2004.
The mode of operation of turbopump unit and arrangement for its
realization, protected by the RF patent
¹ 2225946
(application ¹
2002113441 dated 23.05.2002),has been developed.
The patent is published in
the bulletin "Inventions. Utility models",¹ 8, 2004.
The heat accumulator for heating of working fluid,protected
by the RF patent
¹ 2224187
(application ¹
2002117931 dated 20.02.2002),has been developed.
The patent is published in
the bulletin "Inventions. Utility models",¹ 5, 2004.
Cup-slot sealing of the rotor is developed.
It is protected by the RF patent
¹ 2220345
(application ¹
2002107065 dated 21.03.2002). The patent was published in
the bulletin "Inventions. Utility models", ¹ 36, 2003.
The method for filling of thermal control systems of the spacecraft with
two-phase heat carrier and the device for realization
thereof have been developed.
The method is protected by RF patent
¹ 2214350
(application ¹
2002111641 dated 06.05.2002). The patent is published in
the bulletin "Inventions. Utility models", ¹ 29, 2003.
A method of energy consumption reduction at seawater desalination
has been developed.
The method is protected by RF patent
¹ 2213061
(application ¹
2002129257 dated 04.11.2002). The patent is published in
the bulletin "Inventions. Utility models", ¹ 27, 2003.
A new method is developed for gas analysis of component mixture.
The method is protected by RF patent
¹ 2206081
(application ¹
2001134246 dated 20.12.2001). The patent is published in
the bulletin "Inventions. Utility models", ¹ 16, 2003.
The centrifugal pump protected by RF patent
¹ 2202053
(application ¹
2000121026 dated 15.08.2000) has been developed. The patent is published in
the bulletin "Inventions. Utility models", ¹ 10, 2003.
The method for measurement of electric propulsion thrust (variants) and
device for its realization, protected by RF patent
¹ 2204814
(application ¹
2001131128 dated 20.11.2001),have been developed.The patent is published in
the bulletin "Inventions. Utility models", ¹ 14, 2003.
A membrane installation, protected by RF patent
¹ 2198018
(application ¹ 2001125975 dated 24.09.2001),has been developed.
The patent is published in
the bulletin "Inventions. Utility models", ¹ 4, 2003.
A method of water extraction from air and a device for its realization
were developed. They are protected by RF patent
¹ 2191868
(application ¹ 2001121459 dated 01.08.2001).The patent was published in
bulletin "Inventions.Utility models", ¹ 30, 2002.
Solar thermal propulsion engine and process of its operation
were developed. They are protected by RF patent
¹ 2197630
(application ¹ 2002106714 dated 15.03.2002).The patent was published in
bulletin "Inventions.Utility models", ¹ 3, 2003.
Combustion chamber of liquid rocket engine has been developed,
it is protected by RF Patent¹ 2196917
(application ¹ 2002102796 dated 06.02.2002).The patent was published in
bulletin "Inventions.Utility models", ¹ 2, 2003.
A principle of liquid propellant rocket engine operation and a liquid
propellant rocket engine are developed which are protected by RF patent
¹ 2187684(application ¹
2000124910 dated 03.10.2000).The patent was published in
bulletin "Inventions.Utility models", ¹ 23, 2002(in Russian).
A heat accumulator for heating gases is developed which is protected by RF
patent
¹ 2176767(application ¹
20001120236/06 dated 13.10.2001).The patent was published in
bulletin "Inventions", ¹ 34, 2001.
Construction for nonvented cryogen storage
has been developed. It is covered by
RF patent ¹ 2027944 (application ¹
5054917 dated 16.07.1992).The patent was published in
bulletin "Inventions", ¹ 3, 1995.
Method for the fuel feed to the thermal engine chamber and
device for its realization has been developed. It is covered by
RF patent ¹ 2145039 (application ¹
99105296/06 dated 18.03.1999). The patent was published in
bulletin "Inventions", ¹ 3, 2000.
The facility for plasma injection into ionosphere has been
developed. It is covered by RF patent
¹ 1778916 (application ¹
4872248/25 dated 11.10.1900). The patent was published in
bulletin "Inventions", ¹ 44, 1992.
Method for film cooling of liquid-propellant rocket engine
chamber and a device for its realization (versions) has been
developed. It is covered by RF patent ¹ 2135809 (application ¹
98101859/06 dated 03.02.1998). The patent was published in
bulletin "Inventions", ¹ 24, 1999.
Combustion chamber (version) has been developed. It is covered
by RF patent ¹ 2120560 (application ¹
97112747/06 dated 06.08.1997). The patent was published in
bulletin "Inventions", ¹ 29, 1998.
Method of liquid-propellant rocket engine operation and liquid-propellant
rocket engine has been developed. It is covered by RF patent ¹ 2116491 (application ¹
96106610/06 dated 26.03.1996). The patent was published in
bulletin "Inventions", ¹ 21, 1998.
The technique for generation of luminous
artifical structures in terrestrial space has been developed. It
is covered by RF patent ¹ 2150798
(application ¹ 99103562/06 dated 23.02.1999). The patent was
published in bulletin "Inventions", ¹ 16, 2000.
The facility for the active influence on the
terrestrial ionosphere has been developed. It is covered by RF
patent ¹ 2131176 (application ¹
98105082/25 dated 31.03.1998). The patent was published in
bulletin "Inventions", ¹ 15, 1999.
Facility for active influence on the Earth ionosphere by
plasma injection has been developed. It is covered by RF patent
¹ 2126611 (application ¹
98103616/25 dated 12.03.1998). The patent was published in
bulletin "Inventions", ¹ 5, 1999.
The plasma accelerator with closed electron drift has been
developed. It is covered by RF patent
¹ 2139646 (application ¹
98106621/06 dated 18.03.1998). The patent is published in
bulletin "Inventions",¹ 28, 1999
The heat accumulator for gas heating has been developed. It is
covered by RF patent ¹ 2150054
(application ¹ 99121111/06 dated 07.10.1999). The patent is published in bulletin "Inventions",
¹ 15, 2000.
The solar thermal rocket tngine has been developed. It is
covered by RF patent ¹ 2126493
(application ¹ 98103994/06 dated 18.03.1998).
The patent is published in bulletin "Inventions",
¹ 5, 1999.
The installation for testing the
samples of the materials and elements of the constructions in
liquid or gaseous oxygen with modeling full-scale operating
conditions has been made. It is covered by RF patent ¹ 2166187
(application ¹ 99115670 dated 14.07.1999). The patent is published in
bulletin "Inventions and useful models", ¹ 12, 2001.
The installation for stand
testing discharge performance of hydraulic resistance has been
made. It is covered by RF patent ¹ 2164667 (application ¹
99113272 dated 17.06.1999). The patent is published in bulletin
"Inventions and useful models", ¹ 11, 2001.
The combustion chamber for
sustainer LRE is developed. It is covered by RF patent
¹ 2126905 (application ¹
98104810/06 dated 12.03.1998). The patent was published in
bulletin "Inventions", ¹ 6,1999.
Program packages
AnaSynR System of multifunctional computer
simulation of LRE
AnaSyn application package is intended for the analysis and synthesis of
various cycle of liquid-propellant rocket engines (LRE) at the stage
of concept development and selection of main parameters.
Applied software package
Certificate of registration of computer program ¹ 200161744.
Published in the Bulletin ¹ 19 (38).
Tel: 7 495 456-4608
Fax: 7 495 456-8228
E-mail: kerc@elnet.msk.ru
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