- MagBeam
-
MagBeam is the name given to an ion propulsion system for space travel initially proposed by Professor Robert Winglee of the Earth and Space Sciences Department at the University of Washington for the October 2004 meeting of the NIAC.[1] MagBeam is different from a traditional electrostatic ion thruster in several ways, the primary one being that instead of the fuel and propulsion system being part of the payload craft, they are instead located on a platform held in orbit.
Propulsion system
MagBeam propulsion uses a helicon plasma source to produce a plasma beam. A helicon drive consists of a quartz tube wrapped in a radio antenna, into which a gas such as argon or xenon is injected. RF currents pass through the antenna creating a rapid variation of the electric field, ionizing the gas. The ionized gas is accelerated by a magnetic field to produce thrust. The helicon drive produces a tight beam of ions as the magnetic field that accelerates them continuously expands with the plasma beam keeping them focused. This ion beam is used to push a payload which is equipped with a small amount of gas for propellant such as argon or xenon, a power source and a set of electromagnets to produce a mini-magnetosphere magnetic sail. The gas propellant is ejected into the plasma beam being directed at the craft which heats and ionizes it.
The electromagnets repel this ionized gas imparting thrust upon the payload. This results in an acceleration of around 1 ms-2[citation needed], much faster than traditional ion propulsion systems. This amount of acceleration would make it possible to make a trip to Mars in as little as 50 days, reaching speeds as high as 20 km/s. The deceleration is accomplished by having another platform at the other end of the journey directing a plasma beam at the payload. By eliminating the mass of the propulsion system from the payload the MagBeam system allows for much faster acceleration and higher top speeds than conventional propulsion systems mounted on the payload. One problem with the system is a sufficiently energy dense power-source, with a massive battery bank being proposed for an Earth-Mars Mag-Beam facility massing some 3,000 tons.
The system proposed by Winglee would allow a round-trip from Earth to Mars in 90 days, with 11 days stop-over at Mars.[2]
A similar system for use of a particle beam to push a mini-magnetosphere magnetic sail was proposed by Geoffrey A. Landis in 2001 as a possible propulsion system for interstellar travel.[3]
References
- ^ Celeste Biever "Magnetic beams could power swifter spacecraft", New Scientist, 18 October 2004
- ^ University of Washington, New propulsion concept could make 90-day Mars round trip possible, Oct. 14, 2004
- ^ G. A. Landis, "Interstellar Flight by Particle Beam," STAIF Conference on Innovative Transportation Systems for Exploration of the Solar System and Beyond, Albuquerque NM, Feb. 11-15, 2001. AIP Conference Proceedings Volume 552, 393-396. See also Acta Astronautica, Volume 55, Issue 11, December 2004, Pages 931-934 (link)
External links
Spacecraft propulsion Chemical
rocketsStatePropellantsLiquid propellants (Cryogenic · Hypergolic) · Monopropellant · Bipropellant (Staged combustion cycle · Expander cycle · Gas-generator cycle · Pressure-fed cycle) · TripropellantElectrical
thrustersElectrostaticElectromagneticElectrothermalOtherNuclear
propulsionClosed systemOpen systemOther Categories:- Spacecraft propulsion
- Magnetic propulsion devices
- Spacecraft stubs
Wikimedia Foundation. 2010.
