Category:Optical bistability - GHN: IEEE Global History Network

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		Revision as of 16:01, 20 November 2012 (view source)
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		Latest revision as of 18:29, 4 March 2013 (view source)
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− IEEE GHN Category + The attribute of certain optical devices where two resonant transmissions states or possible and stable depending on the input
− [[File:Optical Bistability Satelite Three Axis Stabilization.jpg|200px|thumb|right|A 1999 photo of The Lunar Prospector designed for a low polar orbit investigation of the Moon. The Lunar Prospector was stabilized by a spin axis with three fuel tanks mounted within a pressurized drum and was controlled by six hydrazine monopropellant 22- Newton thrusters - Image and Information by NASA, G.Scott Hubbard, William Feldman, Mario Acuna, Robert Lin,Alan Binder, and Alex Konopliv.]] + 
    
  [[Category:Electrooptic_effects|{{PAGENAME}}]]   [[Category:Electrooptic_effects|{{PAGENAME}}]]
Latest revision as of 18:29, 4 March 2013
The attribute of certain optical devices where two resonant transmissions states or possible and stable depending on the input





Pages in category "Optical bistability"
This category contains only the following page.
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Retrieved from "http://www.ieeeghn.org/wiki6/index.php/Category:Optical_bistability"
Category: Electrooptic effects
										
									
									
								
																
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+The attribute of certain optical devices where two resonant transmissions states or possible and stable depending on the input
-[[File:Optical Bistability Satelite Three Axis Stabilization.jpg|200px|thumb|right|A 1999 photo of The Lunar Prospector designed for a low polar orbit investigation of the Moon. The Lunar Prospector was stabilized by a spin axis with three fuel tanks mounted within a pressurized drum and was controlled by six hydrazine monopropellant 22- Newton thrusters - Image and Information by NASA, G.Scott Hubbard, William Feldman, Mario Acuna, Robert Lin,Alan Binder, and Alex Konopliv.]]
 [[Category:Electrooptic_effects|{{PAGENAME}}]]

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