Published December 31, 2008 | Version v1
Journal article

Laboratory Facility for Simulating Solar Wind Sails

  • 1. JST/CREST, Kawaguchi, Saitama, 332-0012 (Japan)
  • 2. Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510 (Japan)
  • 3. Graduate University for Advanced Studies, Sagamihara, Kanagawa, 229-8510 (Japan)
  • 4. Tokai University, Hiratsuka, Kanagawa, 259-1292 (Japan)
  • 5. Kyoto University, Uji, Kyoto, 611-0011 (Japan)

Description

Magnetic sail (MagSail) is a deep space propulsion system, in which an artificial magnetic cavity captures the energy of the solar wind to propel a spacecraft in the direction leaving the sun. For a scale-model experiment of the plasma flow of MagSail, we employed a magnetoplasmadynamic arcjet as a solar wind simulator. It is observed that a plasma flow from the solar wind simulator reaches a quasi-steady state of about 0.8 ms duration after a transient phase when initiating the discharge. During this initial phase of the discharge, a blast-wave was observed to develop radially in a vacuum chamber. When a solenoidal coil (MagSail scale model) is immersed into the quasi-steady flow where the velocity is 45 km/s, and the number density is 1019 m-3, a bow shock as well as a magnetic cavity were formed in front of the coil. As a result of the interaction between the plasma flow and the magnetic cavity, the momentum of the simulated solar wind is decreased, and it is found from the thrust measurement that the solar wind momentum is transferred to the coil simulating MagSail.

Additional details

Identifiers

Publishing Information

Journal Title
AIP Conference Proceedings
Journal Volume
1084
Journal Issue
1
Journal Page Range
p. 754-759
ISSN
0094-243X
CODEN
APCPCS

Conference

Title
26. international symposium on rarified gas dynamics
Dates
20-25 Jul 2008
Place
Kyoto (Japan)

Optional Information

Notes
(c) 2009 American Institute of Physics