Study on Acoustic Prediction and Reduction of Epsilon Launch Vehicle at Liftoff-Reference-Cited by-同舟云学术

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Study on Acoustic Prediction and Reduction of Epsilon Launch Vehicle at Liftoff

Published:2015-03 Issue:2 Volume:52 Page:350-361
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Tsutsumi S.¹,Ishii T.²,Ui K.³,Tokudome S.⁴,Wada K.⁵

Affiliation:

1. JAXA's Engineering Digital Innovation (JEDI) Center, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan

2. Institute of Aeronautical Technology, Japan Aerospace Exploration Agency, Chofu, Tokyo 182-8522, Japan

3. Space Transportation Mission Directorate, Japan Aerospace Exploration Agency, Tsukuba, Ibaraki 305-8505, Japan

4. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan

5. Science Service, Inc., Chuuou-ku, Tokyo 103-0012, 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.A33010

Reference38 articles.

1. EldredK. M.JonesG. W. “Acoustic Loads Generated by the Propulsion System,” NASA SP-8072, June 1971.

2. Experimental Study and Simulation of Rocket Engine Freejet Noise

3. Measurements of Unsteady Pressures near the Plume of a Solid Rocket Motor

4. Modifications to the NASA SP-8072 Distributed Source Method II for Ares I Lift-Off Environment Predictions

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