“…In a series of theoretical and experimental investigations on MagSail and its derivatives at JAXA and in collaboration with Japanese universities, Funaki et al [8][9][10][11][12] have lead research work in magnetic sails and propulsion systems that utilize magnetic field (revised M2P2 or magneto-plasmasail/MPS). The first laboratory experiment of MagSail was conducted to confirm theoretically derived thrust formula.…”
Section: Fundamental Physical Principlesmentioning
confidence: 99%
“…In addition to the spacecraft guidance method in a radial acceleration [31], electromagnet system should be studied in detail; until now, only rough estimations are conducted [9,32,33]. The principle of magneto-plasma sailing with magnetic field inflation by plasma injection developed by Funaki et al [8][9][10][11][12], Yamakawa et al [34], and Ashida et al [35], is shown in Fig. 4.…”
Section: Fundamental Physical Principlesmentioning
confidence: 99%
“…where r Li = 72 km if m i = 1.67 × 10 −27 kg, u sw = 400 km/s, e = 1.6 × 10 −19 C, and B mp = 29 nT [8,9,11,38,39,42]. At a given value of v ⊥ , the Larmor radius at which the particle will gyrate will be…”
Section: Scaling Parameter Of Magsailmentioning
confidence: 99%
“…Defining characteristic length of the magnetosphere as L, so that S = π L 2 , correlation between L and F is derived. One may notice that about L = 10 km is required to obtain 1 N, which will be suitable for a 1000-kg-class deep space explorer [8,11,34,32].…”
Section: System Of Forces Acting On the Spacecraft Due To The Sun Andmentioning
confidence: 99%
“…Since there is no need to deploy large mechanical structures, one potential significant benefit of the M2P2 is its small hardware size. Research groups in Japan, among others those led by Funaki, have also carried out significant work in magnetic sail propulsion systems [8][9][10][11][12]. The design of the magnetic sail type space propulsion has steadily evolved over time, and the first magnetic sail spacecraft model has been created [13][14][15][16].…”
A solar magnetic sailing spacecraft utilizes the interaction between solar wind and magnetic field that is generated by a loop of superconducting wire attached onboard of the spacecraft. The development of the working principle of solar magnetic sailing from MagSail to magnetospheric plasma propulsion and magneto-plasma-sail is reviewed and discussed to study their performance, focusing on its operation for interplanetary travel. The orbital dynamic of MagSail is elaborated to explore the probable trajectories of interest for space travel. Examples for MagSail interplanetary travel are discussed for insight and future continuing work.
“…In a series of theoretical and experimental investigations on MagSail and its derivatives at JAXA and in collaboration with Japanese universities, Funaki et al [8][9][10][11][12] have lead research work in magnetic sails and propulsion systems that utilize magnetic field (revised M2P2 or magneto-plasmasail/MPS). The first laboratory experiment of MagSail was conducted to confirm theoretically derived thrust formula.…”
Section: Fundamental Physical Principlesmentioning
confidence: 99%
“…In addition to the spacecraft guidance method in a radial acceleration [31], electromagnet system should be studied in detail; until now, only rough estimations are conducted [9,32,33]. The principle of magneto-plasma sailing with magnetic field inflation by plasma injection developed by Funaki et al [8][9][10][11][12], Yamakawa et al [34], and Ashida et al [35], is shown in Fig. 4.…”
Section: Fundamental Physical Principlesmentioning
confidence: 99%
“…where r Li = 72 km if m i = 1.67 × 10 −27 kg, u sw = 400 km/s, e = 1.6 × 10 −19 C, and B mp = 29 nT [8,9,11,38,39,42]. At a given value of v ⊥ , the Larmor radius at which the particle will gyrate will be…”
Section: Scaling Parameter Of Magsailmentioning
confidence: 99%
“…Defining characteristic length of the magnetosphere as L, so that S = π L 2 , correlation between L and F is derived. One may notice that about L = 10 km is required to obtain 1 N, which will be suitable for a 1000-kg-class deep space explorer [8,11,34,32].…”
Section: System Of Forces Acting On the Spacecraft Due To The Sun Andmentioning
confidence: 99%
“…Since there is no need to deploy large mechanical structures, one potential significant benefit of the M2P2 is its small hardware size. Research groups in Japan, among others those led by Funaki, have also carried out significant work in magnetic sail propulsion systems [8][9][10][11][12]. The design of the magnetic sail type space propulsion has steadily evolved over time, and the first magnetic sail spacecraft model has been created [13][14][15][16].…”
A solar magnetic sailing spacecraft utilizes the interaction between solar wind and magnetic field that is generated by a loop of superconducting wire attached onboard of the spacecraft. The development of the working principle of solar magnetic sailing from MagSail to magnetospheric plasma propulsion and magneto-plasma-sail is reviewed and discussed to study their performance, focusing on its operation for interplanetary travel. The orbital dynamic of MagSail is elaborated to explore the probable trajectories of interest for space travel. Examples for MagSail interplanetary travel are discussed for insight and future continuing work.
The analysis of effectiveness of devices with permanent magnets implementation for the space debris objects deorbiting from Law Earth Orbits has been carried out. The deorbit time of space debris objects from Law Earth Orbits with using different mathematical models of interaction of space object own magnetic fields with dynamic flux of ionospheric plasma, has been calculated. The design features of devices with permanent magnets for deorbiting of space debris objects from Law Earth Orbit has been considered.
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