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Study on the Trajectory Design of Ultra-long-range RocketChinese Full Text

Xu Qin;Liu Kun;Song Qiang;Zhang Shu-hui;National University of Defense Technology;Beijing Institute of Aerospace Systems Engineering;

Abstract:Several techniques are applied by ultra-long-range rocket whose range exceeds half of the earth’s circumference, such as high trajectory, partial orbit and etc. Trajectory features of 5 mission schemes are analyzed in this paper, including direct flight, ascent maneuver flight, descent maneuver flight, LEO circular orbit maneuver flight, LEO elliptical orbit maneuver flight. Principal trajectory parameters and key index of maneuver stages are compared.
  • Series:

    (C) Architecture/ Energy/ Traffic/ Electromechanics, etc

  • Subject:

    Aeronautics and Astronautics Science and Engineering

  • Classification Code:

    V412.1

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