RTU Zinātniskās darbības rezultāti un resursi: Personāls

Informācija par autoru

Vārds, Uzvārds:

Sergey Kravchenko

Struktūrvienība:

(25101) Aeronautikas tehnoloģiju katedra

Zinātniskais grāds:

Doktors

E-pasts:

sergey(at)cvsys.eu

Publikācijas

Atrasti 34 rezultāti tiek attēloti no 1 līdz 10.

Analysis of Suitability of Fixed-wing Aircraft for Launching Satellites into Low Earth Orbit
(2024)

Zvignev Koruba, Nikolajs Kuļešovs, Sergey Kravchenko, Vladimirs Šestakovs
Zinātniskais raksts, kas indeksēts Web of science un/vai Scopus datu bāzē

Methodological Approaches to the Design of a Mobile Test Facility Simulating the Outer Space
(2023)

Nikolajs Kuļešovs, Sergey Kravchenko, Ilmārs Blumbergs, Raivis Kubuliņš, Vladimirs Šestakovs
Zinātniskais raksts, kas indeksēts Web of science un/vai Scopus datu bāzē

Acoustic Emission Method as a Means of Quality Control in Multilayer Welding of Thick-Walled Welded Joints
(2023)

Kristīne Carjova, Mukharbiy Banov, Leonīds Vinogradovs, Sergey Kravchenko, Guntis Strautmanis
Zinātniskais raksts, kas indeksēts Web of science un/vai Scopus datu bāzē

Some Results of the Mobile Space Testing Facility Metamorphosis Prototype Design, Development and Test
(2023)

Sergey Kravchenko, Nikolajs Kuļešovs, Ilmārs Blumbergs, Natalia Kravchenko, Vladimirs Šestakovs, Daria Panova, Aya Mahmoud Abdallah Mohamed Medany
Zinātniskais raksts, kas indeksēts Web of science un/vai Scopus datu bāzē

Analysis of the Winged Air Vehicles Features Applicability for Launching Satellites into Low Earth Orbit
(2022)

Nikolajs Kuļešovs, Sergey Kravchenko, Vladimirs Šestakovs, Zbigniew Satnislaw Koruba
Raksts konferenču tēžu krājumā

Some Features of the Space Technology Elements Test in the Specialized Thermal Vacuum Test Facilities
(2022)

Sergey Kravchenko, Nikolay Kuleshov, Vladimirs Šestakovs, Rafal Chatys
Raksts konferenču tēžu krājumā

Development of Electric Propulsion Thrusters Cooling Systems for Perspective Spacecrafts
(2021)

Sergey Kravchenko
Promocijas darbs

Problem of Measuring Thermal Conductivity of Polyurethane Thermal Insulation of Liquid Hydrogen Tanks for Launch Vehicle in Operational Environment
(2021)

Sergey Kravchenko, Nikolajs Kuļešovs, Natalia Panova, Ugis Cabulis, Romass Pauliks, Sergejs Bratarčuks, Vladimirs Šestakovs
Publikācijas konferenču materiālos, kas ir indeksēti Web of Science un/vai SCOPUS

Modeling the Overall, Mass and Aerodynamic Characteristics of the First and Second Stages of the System for Launching Micro- and Nanosatellites into Low Earth Orbits
(2021)

Nikolajs Kuļešovs, Sergey Kravchenko, Vladimirs Šestakovs, Ilmārs Blumbergs, Dmitrijs Titovs, Natalia Panova
Citas publikācijas konferenču (arī vietējo) ziņojumu izdevumos

Comparative Analysis of Possible Aircraft Payload Transportation Method, Suitable for the LatLaunch Reusable Launch Vehicle Operation
(2021)

Sergey Kravchenko, Nikolajs Kuļešovs, Vladimirs Šestakovs, Natalia Panova, Ilmārs Blumbergs
Citas publikācijas konferenču (arī vietējo) ziņojumu izdevumos

Patenti

Atrasti 1 rezultāti tiek attēloti no 1 līdz 1.

Sistēma derīgās kravas nogādei zemes orbītā
LV15679B (20.05.2023.)

Sergey Kravchenko, Nikolajs Kuļešovs, Ilmārs Blumbergs, Natalia Panova, Vladimirs Šestakovs

Projekti

Atrasti 3 rezultāti tiek attēloti no 1 līdz 3.

Aerokosmiskās sistēmas projektēšana un modelēšana piko- un nanosatelītu palaišanai zemes orbītā
Citi

Valdis Avotiņš

Aeronautikas institūts (34-15E00-N7050.4)
Citi

Aleksandrs Urbahs

Aeronautikas institūts (34-25100-N7050.4)

Aleksandrs Urbahs

Informācija par autoru

Publikācijas

Analysis of Suitability of Fixed-wing Aircraft for Launching Satellites into Low Earth Orbit (2024)

Methodological Approaches to the Design of a Mobile Test Facility Simulating the Outer Space (2023)

Acoustic Emission Method as a Means of Quality Control in Multilayer Welding of Thick-Walled Welded Joints (2023)

Some Results of the Mobile Space Testing Facility Metamorphosis Prototype Design, Development and Test (2023)

Analysis of the Winged Air Vehicles Features Applicability for Launching Satellites into Low Earth Orbit (2022)

Some Features of the Space Technology Elements Test in the Specialized Thermal Vacuum Test Facilities (2022)

Development of Electric Propulsion Thrusters Cooling Systems for Perspective Spacecrafts (2021)

Problem of Measuring Thermal Conductivity of Polyurethane Thermal Insulation of Liquid Hydrogen Tanks for Launch Vehicle in Operational Environment (2021)

Modeling the Overall, Mass and Aerodynamic Characteristics of the First and Second Stages of the System for Launching Micro- and Nanosatellites into Low Earth Orbits (2021)

Comparative Analysis of Possible Aircraft Payload Transportation Method, Suitable for the LatLaunch Reusable Launch Vehicle Operation (2021)

Patenti

Sistēma derīgās kravas nogādei zemes orbītā LV15679B (20.05.2023.)

Projekti

Aerokosmiskās sistēmas projektēšana un modelēšana piko- un nanosatelītu palaišanai zemes orbītā Citi

Aeronautikas institūts (34-15E00-N7050.4) Citi

Aeronautikas institūts (34-25100-N7050.4)

Analysis of Suitability of Fixed-wing Aircraft for Launching Satellites into Low Earth Orbit
(2024)

Methodological Approaches to the Design of a Mobile Test Facility Simulating the Outer Space
(2023)

Acoustic Emission Method as a Means of Quality Control in Multilayer Welding of Thick-Walled Welded Joints
(2023)

Some Results of the Mobile Space Testing Facility Metamorphosis Prototype Design, Development and Test
(2023)

Analysis of the Winged Air Vehicles Features Applicability for Launching Satellites into Low Earth Orbit
(2022)

Some Features of the Space Technology Elements Test in the Specialized Thermal Vacuum Test Facilities
(2022)

Development of Electric Propulsion Thrusters Cooling Systems for Perspective Spacecrafts
(2021)

Problem of Measuring Thermal Conductivity of Polyurethane Thermal Insulation of Liquid Hydrogen Tanks for Launch Vehicle in Operational Environment
(2021)

Modeling the Overall, Mass and Aerodynamic Characteristics of the First and Second Stages of the System for Launching Micro- and Nanosatellites into Low Earth Orbits
(2021)

Comparative Analysis of Possible Aircraft Payload Transportation Method, Suitable for the LatLaunch Reusable Launch Vehicle Operation
(2021)

Sistēma derīgās kravas nogādei zemes orbītā
LV15679B (20.05.2023.)

Aerokosmiskās sistēmas projektēšana un modelēšana piko- un nanosatelītu palaišanai zemes orbītā
Citi

Aeronautikas institūts (34-15E00-N7050.4)
Citi