A lightcraft, then, flies on a beam of laser light, turning its energy into thrust. Earlier designs examined the concept from various directions, including one that used a heat-exchanger aboard the rocket and transferred the beamed energy in such a way as to heat a working fluid like hydrogen or ammonia that would be carried onboard. That produces thrust through expansion through a nozzle, much like a chemical rocket.
Another possibility is to carry an onboard solid propellant. But the latest incarnation of the lightcraft operates in dual mode, using air as described above (turned into a plasma by the laser) and then switching to laser thermal rocket mode at higher altitudes (above about thirty kilometers).
The latter concept, of course, demands a small onboard fuel supply, but nothing like the massive fuel/payload ratios we see in today’s rockets. We’re talking about a spin-stabilized, single-stage transportation system to orbit. In its ‘airbreathing’ mode, the engine pulses at a variable rate to achieve what the authors call a ‘quasi-steady thrust,’ one that depends upon the Mach number and altitude along the craft’s flight trajectory.
Monday, September 14, 2009
Laser propulsion to orbit
From ground to orbit. If perfects, it could really drop costs to orbit. [Link]
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