The conceptual design for a laser-riding air-breathing single stage shuttle which would use magnetohydrodynamic (MHD) forces to accelerate the engine working fluid is introduced. A gigawatt powerlevel photon beam delivered from an orbital laser power station is focused by the shuttle craft onto internal engine working fluid to create, within an annular ionization chamber, a confined air plasma stationary wave. Free electrons are immediately pumped from the plasma and ejected into the external slipstream at the perimeter of the machine. The remaining positively charged working fluid is accelerated by gasdynamic expansion and the pinch-plasma effect, and discharged at a rear nozzle. The vehicle slipstream, now negatively charged and conducting, interacts with a concentric positively charged plasma core to provide quasi-steady flight propulsive forces in an externally-excited-field MHD accelerator. Continuous MHD engine electric currents in the near megampere range are attained through the use of: a) remote power ionization of engine working fluid, and b) electron beam space-charge neutralization techniques reported in recent literature on fusion research. A cursory examination of the required laser power, thrust, exhaust velocities, electric current, and working fluid electrical conductivity reveals operable engine parameters in an interesting range indicating that the system may be worthy of further examination.