Blackout Analysis of Small Cone-Shaped Reentry Vehicles-Reference-Cited by-同舟云学术

Blackout Analysis of Small Cone-Shaped Reentry Vehicles

Published:2017-04 Issue:2 Volume:31 Page:269-282
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Ramjatan Sahadeo¹,Magin Thierry²,Scholz Thorsten²,Van der Haegen Vincent²,Thoemel Jan²

Affiliation:

1. University of Florida, Gainesville, Florida 32611

2. von Kármán Institute for Fluid Dynamics, 1640 Rhode-Saint-Genese, Belgium

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.T4825

Reference24 articles.

1. Analysis of an Electromagnetic Mitigation Scheme for Reentry Telemetry Through Plasma

2. HartunianR.StewartG.FergasonS.CurtissT.SeiboldR. “Causes and Mitigation of Radio Frequency (RF) Blackout During Reentry of Reusable Launch Vehicles,” El Segundo Aerospace Rept. ATR-2007(5309)-1, 2007.

3. KimM. K. “Electromagnetic Manipulation of Plasma Layer for Re-Entry Blackout Mitigation,” Ph.D. Dissertation, Univ. of Michigan, Ann Arbor, MI, 2009.

4. RybakJ. P. “Causes, Effects, and Diagnostic Measurements of the Reentry Plasma Sheath,” Colorado State Univ. AFCRL-70-0707, Fort Collins, CO, 1970.

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