Szymon Rafał Krawczuk - Publications - Bridge of Knowledge

Search

Profile photo:  Szymon Rafał Krawczuk

Szymon Rafał Krawczuk

Employment

Filters

total: 11

  • Category
  • Year
  • Options

clear Chosen catalog filters disabled

Catalog Publications

Year 2022
Year 2021
  • A device for measuring heat flux on a rocket skin surface
    Publication

    A novel method for measuring heat flux on a surface is presented. It is an extensive upgrade of currently known heat flux sensors used mostly in civil engineering. As the thermal environment of launchers, especially sounding rocket can have an enormous negative effect on payload, careful considerations have to be taken in the process of preparing insulation. Usually, thermal data provided by the launch vehicle manufacturer is limited...

    Full text available to download

  • Combined environmental testing device for picosatellites
    Publication

    As access to space conditions becomes more available, both technically and economically, scientists’ interest in launching finer and more sophisticated experiments grows. To be qualified for launch, such experiments need to be carefully tested prior to the event. The tests should represent actual launch conditions as closely and in a detailed manner. Typical tests for payload include: vibration tests, thermal and vacuum tests,...

    Full text available to download

  • Investigating lubricants behaviour in microgravity for vibration damping purposes

    Vibration is one of the harshest environments an object is exposed to during and after launch into space on a launch vehicle. Such vibrations should be damped to avoid destruction of the spacecraft or its elements. Currently, active and material damping is used. A possibility of using lubrication as the damping factor is suggested by some research. MoS2 is a typical solid lubricant used in space applications. Its properties vary...

    Full text available to download

  • Sounding rocket vibration mechanical filter and amplifier

    Measuring accelerations and vibrations of a sounding rocket provides both information for engineers on the launcher vehicle performance as well as environment description for future payload designers. Typically, information on the level of vibration and eigenfrequencies are required to properly design a payload. This paper presents a design of a novel mechanical filter and amplifier for mechanical vibrations. Its key feature is...

    Full text available to download

Year 2020
Year 2019
Year 2018

seen 1284 times