Services
Services
Project description
Design and Analytical Support
Design and Analytical Support
THERMAL ANALYSIS
Determination of ILV and aircraft thermal and humidity behavior:
• Analysis of thermal loads: aerodynamic heat fluxes, thermal effects of propulsion system jets;
• Analysis of the thermal condition of aerospace objects at different stages of operation;
• Selection and validation of methods of thermal protection for the structural elements of space launch systems and different types of devices to reenter the atmosphere.
Determination of thermal behavior of ILV launch complex and launch pad structural elements:
• Analysis of thermal loads affecting the launch pad or launcher structure at ILV launch;
• Determination of thermal behavior of the launch support equipment structure being affected by ILV jet impinging at launch.
Determination of ILV and aircraft thermal and humidity behavior:
• Analysis of thermal loads: aerodynamic heat fluxes, thermal effects of propulsion system jets;
• Analysis of the thermal condition of aerospace objects at different stages of operation;
• Selection and validation of methods of thermal protection for the structural elements of space launch systems and different types of devices to reenter the atmosphere.
Determination of thermal behavior of ILV launch complex and launch pad structural elements:
• Analysis of thermal loads affecting the launch pad or launcher structure at ILV launch;
• Determination of thermal behavior of the launch support equipment structure being affected by ILV jet impinging at launch.
Design of thermal control system and spacecraft thermal analysis:
• spacecraft thermal conditions analysis during the orbital flight;
• analysis of the thermal conditions of the individual spacecraft components (onboard equipment and payload units, as well as spacecraft structural elements), spacecraft/orbital objects under thermal vacuum tests;
• simulation of the spacecraft orbital motion and calculation of data required for calculations of the radiation fluxes from the Earth and the Sun;
• development of the spacecraft thermal control systems
Determination of thermal condition of various products and systems:
• Analysis of the thermal condition of various power plants, heating units, heat exchange equipment (boilers, furnaces, etc.).
Procedures that special application package is based on and which are used for thermal analysis of the aerospace technology specimen are proven and found wide application in the engineering practice of Yuzhnoye SDO.
Successful introduction of the thermal analysis into the aerospace technology design process and repeated verification of the analysis results permit to propose this type of engineering services to the potential customers at the engineering services market.
