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The simulations aimed to analyze the analytical solutions for the constant thrust (CT, maximum thrust (MT) if \(p_1=1\) ) arc that would transfer the lander from the initial orbit to the throttle recovery point (TRP) followed by the throttle recovery (TR) phase which ends at the BP terminal point.

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Simulations of Braking Phase Using Analytical Solutions

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  • 发表日期：

    2026年

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  • Dilmurat M. Azimov,
  • Robert H. Bishop

摘要

The simulations aimed to analyze the analytical solutions for the constant thrust (CT, maximum thrust (MT) if \(p_1=1\) ) arc that would transfer the lander from the initial orbit to the throttle recovery point (TRP) followed by the throttle recovery (TR) phase which ends at the BP terminal point.