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Information Seminar Paper

Title

ROCKET COMPLEX WITH ORBITER AND WITH LIQUID PROPELLANT ENGINES ON HIGH CONCENTRATED HYDROGEN PEROXIDE

Pages

  -

Abstract

 THE AUTHOR GIVES A REVIEW OF CRITERIA FOR THE ESTABLISHMENT OF ACTIVE ORBITAL SPACECRAFT, TAKING INTO ACCOUNT THE ANALYSIS OF ASPECTS OF THE APPLICATION OF THE PROPULSION SYSTEM RUNNING ON HYDROGEN PEROXIDE AND THE POSSIBILITY OF HIS RETURN TO THE EARTH SURFACE.AS A RESULT, PROPOSED THE CONCEPT OF CREATING A MODERN TYPE OF SPACECRAFT - MANEUVERING IN ORBIT RETURNING UNMANNED ORBITER IN THE EMBODIMENT OF THE SATELLITE REMOTE SENSING (SRS). IN A PAPER REFLECTS THE RESULTS OF OPTIMIZING THE DESIGN OF THE LAUNCH VEHICLE (LV). ARTICLE EXAMINES THE PRECEDING SCHEMATIC DESIGN ELEMENTS OF SPACE ROCKET COMPLEX. IN PARTICULAR, THE ELEMENTS OF LV, ORBITER, AND THEIR PROPULSION SYSTEMS.CARRIED INITIAL CALCULATIONS AERODYNAMIC PARAMETERS OF ORBITER ON THE DESCENT AND MANEUVERING IN LOW ORBIT.

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    APA: Copy

    Levenko, Oleksandr S., Pauk, Oleg L., & Prisyzhniy, Vladimir I.. (2015). ROCKET COMPLEX WITH ORBITER AND WITH LIQUID PROPELLANT ENGINES ON HIGH CONCENTRATED HYDROGEN PEROXIDE. CONFERENCE OF IRANIAN AEROSPACE SOCIETY. SID. https://sid.ir/paper/945673/en

    Vancouver: Copy

    Levenko Oleksandr S., Pauk Oleg L., Prisyzhniy Vladimir I.. ROCKET COMPLEX WITH ORBITER AND WITH LIQUID PROPELLANT ENGINES ON HIGH CONCENTRATED HYDROGEN PEROXIDE. 2015. Available from: https://sid.ir/paper/945673/en

    IEEE: Copy

    Oleksandr S. Levenko, Oleg L. Pauk, and Vladimir I. Prisyzhniy, “ROCKET COMPLEX WITH ORBITER AND WITH LIQUID PROPELLANT ENGINES ON HIGH CONCENTRATED HYDROGEN PEROXIDE,” presented at the CONFERENCE OF IRANIAN AEROSPACE SOCIETY. 2015, [Online]. Available: https://sid.ir/paper/945673/en

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