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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    General relativity and gravitation 32 (2000), S. 53-77 
    ISSN: 1572-9532
    Keywords: De Sitter spacetime ; particle production
    Source: Springer Online Journal Archives 1860-2000
    Topics: Physics
    Notes: Abstract The complex time WKB (CWKB) approximation has been an effective technique to understand particle production in curved as well as in flat spacetime. Earlier we obtained the standard results on particle production in time-dependent gauge in various curved spacetime, using the method of CWKB. In the present work we generalize the technique of CWKB to the equivalent problems in space-dependent gauge. Using CWKB, we first obtain the gauge invariant result for particle production in Minkowski spacetime in a strong electric field. We then carry out particle production in de Sitter spacetime in space dependent gauge and obtain the same result that we obtained earlier in time dependent gauge. This ensures the gauge invariant description inherent in CWKB. The results obtained for de Sitter spacetime have an obvious extension to particle production in black hole spacetime. It is found that the origin of the Planckian spectrum is due to repeated reflections between the turning points. As mentioned in earlier work, it is now explicitly shown that particle production is accompanied by rotation of currents.
    Type of Medium: Electronic Resource
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  • 2
    Publication Date: 2019-07-13
    Description: This paper provides an overview of the Mars Laser Communications Demonstration Project, a joint project between NASA s Goddard Space Flight Center (GSFC), the Jet Propulsion Laboratory, California Institute of Technology (JPL), and the Massachusetts Institute of Technology Lincoln Laboratory (MIT/LL). It reviews the strawman designs for the flight and ground segments, the critical technologies required, and the concept of operations. It reports preliminary conclusions from the Mars Lasercom Study conducted at MIT/LL and on additional work done at JPL and GSFC. The lasercom flight terminal will be flown on the Mars Telecom Orbiter (MTO) to be launched by NASA in 2009, and will demonstrate a technology which has the potential of vastly improving NASA s ability to communicate throughout the solar system.
    Keywords: Optics
    Type: Space 2003 Conference and Exposition; Sep 23, 2003 - Sep 25, 2003; United States
    Format: application/pdf
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  • 3
    Publication Date: 2019-08-16
    Description: Tlis paper presents an overview of the preliminary design of both the flight and ground systems of the Optical Communication Demonstration and High-Rate Link Facility which will demonstrate optical communication from the International Space Station to ground after its deployment in October 2002. The overview of the preliminary design of the Flight System proceeds by contrasting it with the design of the laboratory-model unit, emphasizing key changes and the rationale behind the design choices. After presenting the preliminary design of the Ground System, the timetable for the construction and deployment of the flight and ground systems is outlined.
    Keywords: Optics
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  • 4
    Publication Date: 2019-08-15
    Description: Mountain-top to mountain-top optical link experiments have been initiated at JPL, in order to perform a systems level evaluation of optical communications. Progress made so far is reported. ne NASA, JPL developed optical communications demonstrator (OCD) is used to transmit a laser signal from Strawberry Peak (SP), located in the San Bernadino mountains of California. This laser beam is received by a 0.6 m aperture telescope at JPL's Table Mountain Facility (TMF), located in Wrightwood, California. The optical link is bi-directional with the TMF telescope transmitting a continuous 4-wave (cw) 780 run beacon and the OCD sending back a 840 nm, 100 - 500 Mbps pseudo noise (PN) modulated, laser beam. The optical link path is at an average altitude of 2 km above sea level, covers a range of 46.8 km and provides an atmospheric channel equivalent to approx. 4 air masses. Average received power measured at either end fall well within the uncertainties predicted by link analysis. The reduction in normalized intensity variance (sigma(sup 2, sub I)) for the 4-beam beacon, compared to each individual beam, at SP, was from approx. 0.68 to 0.22. With some allowance for intra-beam mis-alignment, this is consistent with incoherent averaging. The sigma(sup2, sub I) measured at TMF approx. 0.43 +/- 0.22 exceeded the expected aperture averaged value of less than 0.1, probably because of beam wander. The focused spot sizes of approx. 162 +/- 6 microns at the TMF Coude and approx. 64 +/- 3 microns on the OCD compare to the predicted size range of 52 - 172 microns and 57 - 93 microns, respectively. This is consistent with 4 - 5 arcsec of atmospheric "seeing". The preliminary evaluation of OCD's fine tracking indicates that the uncompensated tracking error is approx. 3.3 micro rad compared to approx. 1.7 micro rad observed in the laboratory. Fine tracking performance was intermittent, primarily due to beacon fades on the OCD tracking sensor. The best bit error rates observed while tracking worked were 1E-5 to 1E-6.
    Keywords: Optics
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