RTU Research Outputs and Resources: Reasearch Staff

Information about Author

Name, Surname:

Sergey Kravchenko

Department:

(25101) Aeronautikas tehnoloģiju katedra

Scientific Degree:

Doktors

E-mail:

sergey(at)cvsys.eu

Publications

34 items found, displaying 1 to 10.

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

Zvignev Koruba, Nikolajs Kuļešovs, Sergey Kravchenko, Vladimirs Šestakovs
Scientific article indexed in SCOPUS or WOS database

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
Scientific article indexed in SCOPUS or WOS database

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
Scientific article indexed in SCOPUS or WOS database

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
Scientific article indexed in SCOPUS or WOS database

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
Conference paper

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

Sergey Kravchenko, Nikolay Kuleshov, Vladimirs Šestakovs, Rafal Chatys
Conference paper

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

Sergey Kravchenko
Doctoral Thesis

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
Full-text conference paper published in conference proceedings indexed in SCOPUS or WOS database

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
Full-text conference paper published in other conference proceedings

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
Full-text conference paper published in other conference proceedings

Patents

2 items found, displaying 1 to 2.

The first stage of the satellite carrier droppable from the platform aircraft, which is a twin-boom winged air vehicle
LV15680B (20.09.2023.)

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

System for payload launching into a low-earth orbit
LV15679B (20.05.2023.)

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

Projects

3 items found, displaying 1 to 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

Information about Author

Publications

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)

Patents

The first stage of the satellite carrier droppable from the platform aircraft, which is a twin-boom winged air vehicle LV15680B (20.09.2023.)

System for payload launching into a low-earth orbit LV15679B (20.05.2023.)

Projects

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)

The first stage of the satellite carrier droppable from the platform aircraft, which is a twin-boom winged air vehicle
LV15680B (20.09.2023.)

System for payload launching into a low-earth orbit
LV15679B (20.05.2023.)

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

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