2006
DOI: 10.2514/1.16391
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Lower Hybrid Instability in Gas-Dust Formations from Rocket Exhaust in the Ionosphere

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Cited by 8 publications
(5 citation statements)
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“…Later, Rosenberg et al (1999) considered a lower hybrid (LH) instability driven by a beam of negatively charged dust streaming across B, finding that this instability could be relevant for explaining the enhanced radar backscatter from space shuttle exhaust. Rosenberg and Sorasio (2006) have considered the possibility of LH instability in dust-gas formations from rocket exhausts injecting combustion products into the ionosphere (see Platov 2004). …”
Section: Possible Instabilities In the Earth' S Ionospherementioning
confidence: 99%
“…Later, Rosenberg et al (1999) considered a lower hybrid (LH) instability driven by a beam of negatively charged dust streaming across B, finding that this instability could be relevant for explaining the enhanced radar backscatter from space shuttle exhaust. Rosenberg and Sorasio (2006) have considered the possibility of LH instability in dust-gas formations from rocket exhausts injecting combustion products into the ionosphere (see Platov 2004). …”
Section: Possible Instabilities In the Earth' S Ionospherementioning
confidence: 99%
“…The exhaust plume from solid rocket motors can be characterized as weakly ionized dusty plasma, which contains a large numbers of aluminum oxide particles (Al 2 O 3 ) [16,17]. Plasma and dust parameters of the rocket exhaust measured by experiments (Refs.…”
Section: Numerical Results and Discussionmentioning
confidence: 99%
“…The parameters chosen in the simulation are as follows: B ∼ 5 × 10 −5 T, n e ∼ 0.994 × 10 5 cm −3 , n i ∼ 1.0 × 10 5 cm −3 , n d ∼ 0.006n i , T e ∼ 0.2 eV, T d = T i ∼ 0.1 eV, Z d ∼ 50 and m d ∼ 4 × 10 9 m p , where m p is the proton mass (Mendis & Rosenberg 1994). The dust particles are injected into the background plasma with a speed u d0 ∼ 2 km s −1 (Huba et al 2000;Rosenberg & Sorasio 2006). Then we obtain ω pe = 1.50 × 10 7 rad s −1 , ω pi = 0.93 × 10 5 rad s −1 , ω pd = 25.50 rad s −1 , Ω ce = 8.79 × 10 6 rad s −1 , Ω ci = 0.24 × 10 3 rad s −1 and Ω cd = 5.99 × 10 −5 rad s −1 .…”
Section: Numerical Simulation Resultsmentioning
confidence: 99%
“…The interaction between rocket exhausts and the background plasma has received growing interest owing to the potential role in the ionosphere (Fried & Conte 1963;Seiler, Yamada & Ikezi 1976;Shukla 1992;Mendis & Rosenberg 1994;Rosenberg & Krall 1994;Bernhardt et al 1995;Bharuthram & Singh 1997;Bharuthram & Rosenberg 1998;Rosenberg, Salimullah & Bharuthram 1999;Huba, Joyce & Fedder 2000;Scales & Ganguli 2004;Rosenberg & Sorasio 2006;Rosenberg, Bernhardt & Clark 2011;Bernhardt et al 2012;Chen 2016;Liu et al 2021). In a recent paper, Bernhardt et al (1995) have studied possible mechanisms for enhanced radar backscatter from space shuttle exhaust in the ionosphere.…”
Section: Introductionmentioning
confidence: 99%
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