AIAA Atmospheric Flight Mechanics Conference and Exhibit 2007
DOI: 10.2514/6.2007-6633
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Implications and Mitigation of Radio Frequency Blackout During Reentry of Reusable Launch Vehicles

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Cited by 110 publications
(105 citation statements)
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“…From a physical perspective, the electron density should follow the distribution that it goes to zero near the plasma-air interface and reaches the maximum in a limited distance from one interface, which have been validated and adopted by many researchers [2, 3, 10-12, 14, 15, 17]. The experiments about the plasma sheath [10,11] show that the electron density profile for plasma objects may follow a biexponential curve. Therefore, the bi-exponential function distribution will be adopted for our EM problem model, which can be expressed as…”
Section: The Electron Density Distribution For the Proposed Magnetizementioning
confidence: 97%
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“…From a physical perspective, the electron density should follow the distribution that it goes to zero near the plasma-air interface and reaches the maximum in a limited distance from one interface, which have been validated and adopted by many researchers [2, 3, 10-12, 14, 15, 17]. The experiments about the plasma sheath [10,11] show that the electron density profile for plasma objects may follow a biexponential curve. Therefore, the bi-exponential function distribution will be adopted for our EM problem model, which can be expressed as…”
Section: The Electron Density Distribution For the Proposed Magnetizementioning
confidence: 97%
“…In the above, z is the radial distance, N e0 is the peak of electron density, z 10 and z 20 represents the curve's shape, L 1 determines the location where electron density reaches the maximum, and L 2 specifies the thickness of the plasma. In the following simulation, some parameters of (23) are designated as constants, which are: L 1 = 15 cm, L 2 = 60 cm (that is to say, the thickness of the plasma slab is 60 cm), z 10 = 1 cm, z 20 = 4 cm.…”
Section: The Electron Density Distribution For the Proposed Magnetizementioning
confidence: 99%
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“…The propagation of electromagnetic waves through a plasma causes phenomena such as the radio-communication cut-off during spacecraft atmospheric re-entry 6,7 and the attenuation of signals through plasma plumes of modern electric propulsion systems; 8 and it is also used for the sustainment of plasma columns by surface wave 9 and the plasma diagnostics (microwave interferometry). 10 The phenomena of wave absorption/reflection via plasma occur when high-frequency (radiofrequency RF 1-300 MHz and microwaves MW>300 MHz) electromagnetic waves propagate in partially ionized plasmas.…”
Section: -3mentioning
confidence: 99%
“…The ionized gas is called plasma sheath, which leads to the lost or at least severely degraded of the communication, telemetry, and GPS navigation signals. [2][3][4] Radio blackout during the re-entry has puzzled the aerospace industry for decades and has not yet been completely resolved.…”
Section: Introductionmentioning
confidence: 99%