Determining the zone of aerodynamic interference between a descent module and the module’s parachute compartment hatch door during separation

Author:

Kalugin V. T.,Slobodyanuk D. M.

Publisher

AIP Publishing

Reference20 articles.

1. Smirnov, V. Yu. (2010). Aerodynamic compatibility of an aircraft and payload and optimization of the experimental investigation in this area. Scientific herald of the Moscow State Technical University of Civil Aviation, (154).

2. Aerodynamic interference between high-speed slender bodies

3. Uematsu, T., Ishida, T., Aso, S., & Tani, Y. (2009). Reduction of Aerodynamic Interference for Separation of Two-Stage Reusable Launch Vehicles. In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition (p. 1101).

4. Analysis of the aerodynamic impact of the dispenser stance for the separation of cluster munitions

5. Aksenov, A.A., Dyadkin, A.A., Moskalev, I.V., Petrov N.K., & Simakova T. V. (2016). Computer simulation of the flow and the relative motion of the reentry vehicle and the parachute compartment hatch cover in the course of their separation during descent. Space Engineering and Technology, 121, 116–129.

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