Hybrid Continuum/Rarefied Flow Simulations of Plume Interaction with Full-Sized Spacecraft-Reference-Cited by-同舟云学术

Hybrid Continuum/Rarefied Flow Simulations of Plume Interaction with Full-Sized Spacecraft

Published:2022-03 Issue:2 Volume:59 Page:660-673
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Tani Hiroumi¹^ORCID,Ohmaru Tetsufumi²

Affiliation:

1. Japan Aerospace Exploration Agency, Tsukuba 305-8505, Japan

2. Ryoyu Systems Co., Ltd., Tokyo 105-0023, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34882

Reference24 articles.

1. Plume flow and plume impingement in space technology

2. DettleffG.GrabeM. “Basics of Plume Impingement Analysis for Small Chemical and Cold Gas Thrusters,” RTO-AVT/VKI Lecture Series, AVT-194, von Karman Institute, Rhode St. Genèse, Belgium, 2011, pp. 1–40.

3. TribbleA. C.BoyadjianB.DavisJ.HaffnerJ.McCulloughE. “Contamination Control Engineering Design Guidelines for the Aerospace Community,” NASA CR 4740, 1996.

4. DSMC analysis of bipropellant thruster plume impingement on a geostationary spacecraft

5. Effect of nozzle boundary layers on rocket exhaust plumes.

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