AO for high peak power lasers
... 3. No need for an extended field of view (point focus only) 4. Only slow response needed (at present . . .) Things that make AO for high-power lasers harder 1. Too much light (need to protect the wavefront sensor from the laser) 2. Deformable mirror needs to withstand the power density in the beam ...
... 3. No need for an extended field of view (point focus only) 4. Only slow response needed (at present . . .) Things that make AO for high-power lasers harder 1. Too much light (need to protect the wavefront sensor from the laser) 2. Deformable mirror needs to withstand the power density in the beam ...
Preview of Period 3: Electromagnetic Waves – Radiant Energy II
... Communication is the transfer of information Transferring information requires ….. ♦ a source of information (a person or device) ♦ a signal (the information) ♦ a receiver ♦ modulation (changing) of the signal ...
... Communication is the transfer of information Transferring information requires ….. ♦ a source of information (a person or device) ♦ a signal (the information) ♦ a receiver ♦ modulation (changing) of the signal ...
docx - Pdx
... Q14: To produce more frequent stimulated emissions than spontaneous emissions, how do you need to alter the lifetime of each energy level? (Note that you may not be able to verify this by adjusting the lifetime settings yet, but you should be able to answer the question using the information we have ...
... Q14: To produce more frequent stimulated emissions than spontaneous emissions, how do you need to alter the lifetime of each energy level? (Note that you may not be able to verify this by adjusting the lifetime settings yet, but you should be able to answer the question using the information we have ...
AS301, IITM, Lecture 8 (22/08/2007)
... (eg. Nuclear or solar) is used, hence much higher propellant energy is possible. The electric rocket engine is a device that converts electric power into a forward-directed force or thrust by accelerating an ionized propellant (i.e., mercury, cesium, argon, or xenon) to a very high exhaust velocity. ...
... (eg. Nuclear or solar) is used, hence much higher propellant energy is possible. The electric rocket engine is a device that converts electric power into a forward-directed force or thrust by accelerating an ionized propellant (i.e., mercury, cesium, argon, or xenon) to a very high exhaust velocity. ...
femtosecond laser ablation of dielectrics
... evolution of the solid is monitored, under conditions where breakdown is achieved and below, with the time-resolved interferometry technique [4] which allows to measure the density of carriers in the solid, and to follow their relaxation. Thanks to its great flexibility, this double pulse technique ...
... evolution of the solid is monitored, under conditions where breakdown is achieved and below, with the time-resolved interferometry technique [4] which allows to measure the density of carriers in the solid, and to follow their relaxation. Thanks to its great flexibility, this double pulse technique ...
Title of PAPER - Department of Physics and Astronomy
... can be reinforced or other materials can be used with a higher melting point to increase the durability of the mirror. Conclusion To summarise, if conductivity and scattering is ignored, lasers with a wavelength of 500 nm and lower will melt a mirror with silver as its optical coating. Different mat ...
... can be reinforced or other materials can be used with a higher melting point to increase the durability of the mirror. Conclusion To summarise, if conductivity and scattering is ignored, lasers with a wavelength of 500 nm and lower will melt a mirror with silver as its optical coating. Different mat ...
laser - SlideBoom
... coherent beam of monochromatic light by laser action. A coherent beam resulted which all of the photons are in phase. ...
... coherent beam of monochromatic light by laser action. A coherent beam resulted which all of the photons are in phase. ...
Photonic laser thruster
A photonic laser thruster is an amplified laser thruster that generates thrust directly from the laser photon momentum, rather than laser-heating propellant. The concept of single-bounce laser-pushed lightsails that utilize the photon momentum was first developed in the 1960s, however, its conversion of laser power to thrust is highly inefficient, thus has been considered impractical. Over 50 years, there had been numerous theoretical and experimental efforts to increase the conversion efficiency by recycling photons, bouncing them repetitively between two reflective mirrors in an empty optical cavity, without success. In December 2006, Young Bae successfully solved this problem and demonstrated the conversion efficiency enhancement by a factor of 100 and a photon thrust of 35 micronewtons by putting the laser energizing media between the two mirrors as in typical lasers, and the photonic laser thruster was born. In August 2015, the photonic laser thruster was demonstrated to increase the conversion efficiency enhancement by a factor over 1,000 and to achieve a photon thrust of 3.5 millinewtons at Y.K. Bae Corporation. In addition, Propelling, slowing and stopping of a small satellite, 1U CubeSat, in simulated zero-gravity were demonstrated. The photonic laser thruster was initially developed for use in nanometer precision spacecraft formation, for forming ultralarge space telescopes and radars. The photonic laser thruster is currently developed for high-precision and high-speed maneuver of small spacecraft, such as formation flying, orbit adjustments, drag compensation, and rendezvous and docking. The photonic laser thruster can be used for beaming thrust from a conventional heavy resource vehicle to a more expensive & lightweight mission vehicle, similar to tankers in aerial refueling.The practical usage of the photonic laser thruster for main space propulsion would require extremely high laser powers and overcoming technological challenges in achieving the laser power and fabricating the required optics. Photonic laser thrusters have a very high specific impulse, and can permit spacecraft reach much higher speeds than with conventional rockets, which are limited by the Tsiolkovsky rocket equation. If the photonic laser thruster is scalable for the use in such main space propulsion, multiple photonic laser thrusters can be used to construct a 'photonic railway' that has been proposed as a potential permanent transport infrastructure for interplanetary or interstellar commutes, allowing the transport craft themselves to carry very little fuel.