A new trajectory design approach for lift-control reentry flight vehicle based on cruising design concept is proposed in this paper. The cruising parameter could be aerodynamic overload, dynamic pressure, or aeroheating rate at stagnation point. For a high speed reentry flight vehicle, based on this trajectory design approach, it could firstly cruise at an appropriate aeroheating rate, then at an appropriate aerodynamic overload, and finally at an appropriate dynamic pressure. As an example, the entry trajectories designed for a certain lift-control reentry vehicle based on the new approach are presented in this paper, too.
A New Reentry Trajectory Design Approach for Lift-control Flight Vehicle Based on Cruising Design Concept
01.08.2018
408989 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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