PLX’s history of newsworthy innovation and problem solving has made it the world’s leader in Hollow Retroreflector and Monolithic Optical Structure Technology™ (M.O.S.T.).
Much of our breakthrough technology is proprietary and customized to fit the needs of such clients as Lockheed Martin, JPL, Raytheon, Northrop Grumman Corporation and cannot be published. However, for more information on how we can help optimize your optical system, call 631-586-4190 and ask for our Director of Engineering, or go to contact us.
Tagsmetrology, interferometry, beam-delivery, boresighting, aerospace, monolithic optics, spectroscopy, space-applications, laser-tracking, monolithic, satellite, MEMS, defense, lidar, targeting, alignment, autocollimation, autocollimator, laser tracking, telescope, laserTracking, inflight-applications, FTIR, environment-monitor, Active Optics, Hybrid;
With their exceptional stability, PLX’s boresighting systems have been repeatedly proven in the field. This paper will expand upon the Monolithic Optical Structure Technology™ (M.O.S.T.) solution with case studies of Monolithic Optical Structure Technology™ (M.O.S.T.) designs and results for specific applications, such as laser delay line systems, boresighting, and telescope alignment systems.
Precision optical alignment capability across a range from the UV to the far-IR and a lighterweight design have long given hollow retroreflectors an advantage over their solid cousins (retroreflector prisms) in boresighting, laser tracking, rangefinding, diverse laboratory applications and even space-based spectrometers.
When two separate bundles of parallel light beams having the same characteristic wavelength and propagation are combined, the combination of the bundles causes a phenomenon called light interference. To create such an interference, Michelson used two mirrors at 90° and a beamsplitter to separate the beams and recombine them. Figure 1 is a schematic of the classical Michelson interferometer.
The studies of the Martian atmosphere and climate have been long time identified as the primaryscientific goal of ExoMars Trace Gas Orbiter (TGO) , which is the follow up of the Mars Science Orbiter concept .