Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
Author:
Affiliation:
1. Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J062135
Reference17 articles.
1. Theoretical Modeling of Two-Body Interaction in Supersonic Flow
2. Abort Separation of Launch Escape System Using Aerodynamic Interference
3. Parametric Study on Aerodynamic Interaction of Supersonic Parachute System
4. Stage-Separation Aerodynamics of Two-Stage Space Transport Systems Part 2: Unsteady Simulation
5. Analysis of inviscid and viscous hypersonic flows past a two-stage spacecraft
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