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EJASA - Part 8Page 50 Even as this is being written, substantial developments are being made in terrestrial video compression techniques for High Definition TeleVision (HDTV). Compression ratios as high as 100:1 have been achieved with only a small reported impairment in perceived video quality. [87] A 100:1 compression ratio would reduced bandwidth required by the digitized video signal by a factor of 100. If it was applied to an ETI interstellar communication system, the effective CNR could be increased by 20 dB. Of course, we cannot yet comment on whether ETIs would use such techniques, or what their level of sophistication is. What we can say, however, is that optical communi- cations technology, along with video compression techniques, would make it much easier to transmit high-quality "real-time" video signals over thousands of light years. What was previously thought possible with old-fashioned analog TV signals and a 1 GW transmitter over ten light years now becomes possible over one hundred light years. ETI signals may be linearly or circularly polarization-modulated, so that as previously mentioned, some means of analyzing the light would be required to detect the modulation. This polarization analyzing system could include a polarizer and a Soleil-Babinet compensator or quarter/half-wave retardation plates. The latter might be spun to cause sampling of all polarization states. If the signals are frequency (or phase) modulated with relatively small deviations, then only the professional heterodyne receiver will be able to recover the modulation envelop, whatever the signal strength. Shopping List - 1. 8"-14" (20-36 cm) or larger Schmidt-Cassegrain with periodic error correction drive and RS-232 or IEEE-488 interface. Low $2,000 High $12,000 2. CCD imaging and tracking system with RS-232 or IEEE-488 interface. Low $1,100 High $3,200 3. Polarizaton analyzer. Low $100 High $2,000 4. Fiber-optic umbilical and connectors (ten meters). Low $150 High $150 5. Triple grating monochromator (resolution 0.1 to 0.01 nm) with RS-232 or IEEE-488 interface. Low $1,000 High $6,500 6. APD photon-counter or photomultiplier front-end. Low $200 High $3,000 EJASA, Vol. 3, No. 6, January 1992 Page 51 7. Front-end cooling system. Low $200 High $1,000 8. PC with fixed (hard) disk and RS-232/IEEE-488 interfaces. Low $1,000 High $3,000 9. Spectrum analyzer PC card or stand-alone 0-10 MHz spectrum analyzer. Low $1,000 High $4,400 10. Video and audio monitors (PC may double-up for this purpose). Low $200 High $200 11. Miscellaneous Low $1,000 High $2,000 12. Labor - Free Total cost: Low $8,000; High $38,000 Thus, the low-end cost is approximately $8,000; less if telescope and computer system are already available. This is an affordable activity for many clubs and societies. Some of the equipment above is optional and may be replaced by less sophisticated devices, e.g., the automatic scanning monochromator could be replaced by a manual monochromator or a series of discrete high-Q bandpass filters, such as a 656 nm H_alpha filter. By omitting the electrical spectrum analyzer and using a fixed optical bandpass filter, instead of a scanning monochromator, the cost of a rudimentary system adaptation to an existing telescope would fall to about $3,000. This figure will be affordable for some individual enthusiasts. Instead of a scanning grating monochromator, a scanning grating spectrometer might be used, where a linear CCD array is employed to produce an essentially instantaneous display of optical spectra (over a limited band) on a video display terminal (VDT). However, this does not allow for the flexibility of employing a single photodetector optimized for bandwidth and photon-counting sensitivity, and thus this approach will be more expensive and/or less sensitive. Often, mono- chromators use triple gratings in order to obtain spectral resolutions of 0.01 nm or better. As previously mentioned, a set of four optical fibers surrounding the signal fiber and corresponding low-bandwidth photodetectors might be used in the system for fine guidance purposes. Within this account of Amateur Optical SETI is the ambitious desire to detect the modulation envelop. Hopefully, the ETI signals will be intensity or polarization-modulated so that the modulation can be detected by an incoherent receiver. For weak signals, we may only Page 52 be able to detect the presence of an optical carrier or beacon (perhaps Signpost SETI) and then only after some signal integration. However, this would be a significant achievement by itself, allowing for more powerful professional receivers to be built later for detecting the modulation envelope. As a spin-off from the MOP, electronic Multi-Channel Spectrum Analyzers (MCSAs) could be developed for the Amateur Optical SETI market, eventually making Amateur Optical SETI an even more affordable activity for optical astronomy clubs and societies. Perhaps ETIs do not expect their signals to be detected until the targeted civili- zations make a collective, cooperative, and systematic search of their home skies! THE MICROWAVE AND OPTICAL OBSERVING PROJECT (MOOP) The following is the author's tentative list of objectives for the optical extension to MOP. It is called the Microwave and Optical Observing Project, otherwise known by the acronym MOOP. Project Goal: To continue the search for microwave (and millimeter wave) signals of extraterrestrial intelligent origin and to extend the search into the infrared and visible spectrums. Project Objectives: 1. To use existing large ground-based optical telescopes to carry out a Targeted Search of about 800 nearby solar-type stars with spectral resolution of 1 kHz and sensitivity 10^-16 W/m^2. For selected laser wavelength bands corresponding to atmospheric windows in the visible and infrared wavelength range (350 nm to 12,000 nm). 2. To use existing large ground-based optical telescopes to carry out a Targeted Search of about 1 million nearby solar-type stars with spectral resolution of 100 kHz and sensitivity 10^-10 W/m^2. For selected laser wavelength bands corres- ponding to atmospheric windows in the visible and infrared wavelength range (350 nm to 12,000 nm). 3. To use dedicated groups of amateur astronomers and coordinate their activities to conduct with their ground-based optical telescopes a low-sensitivity Targeted Search of about 800 nearby solar-type stars with spectral resolution < 1 nm, and sensitivity 10^-16 W/m^2. For selected wavelength bands in the visible and near-infrared wavelength range (350 nm to 1,200 nm). Duration: 2001 - 2010 Cost: $20M for starters. Assumes use of existing large ground- based professional telescopes and the cost of modifying the telescopes for adaptive reception and Optical SETI. Page 53 ========================================================================== Table 5 Nearest stars favored for MOP's 800 star Targeted Search ========================================================================== RGO RH DEC Relative Distance Apparent Spectral Number H M S D M Vel. km/s L.Y. Magnitude Type -------------------------------------------------------------------------- 559A 14 36 11 -60 37.8 -22.2 4.39 -0.01 G2 eye, SB 559B 14 36 11 -60 37.8 -0.0 4.39 1.33 K0 eye 144 3 30 34 -9 37.6 +15.4 10.79 3.73 K2 eye 820A 21 4 40 38 30.0 -64.3 11.01 5.22 K5 eye, AB 820B 21 4 40 38 30.0 -63.5 11.01 6.03 K7 eye 845 21 59 33 -56 59.6 -40.4 11.20 4.69 K4 eye 71 1 41 45 -16 12.0 -16.2 11.77 3.50 G8 eye 380 10 8 19 49 42.5 -26.0 14.68 6.59 K7 166A 4 12 58 -7 43.8 -42.4 15.90 4.43 K1 eye 702A 18 2 56 2 30.6 -7.2 16.72 4.03 K0 eye, UD 702B 18 2 56 2 30.6 -10.0 16.72 6.00 K5 eye, SB 663A 17 12 16 -26 31.8 -0.7 17.25 4.32 K0 eye 663B 17 12 16 -26 31.9 -0.2 17.25 5.10 K1 eye 570A 14 54 32 -21 11.5 +19.5 18.11 5.78 K5 eye 664 17 13 9 -26 28.6 -1.3 18.31 6.34 K5 783A 20 7 55 -36 13.7 -130.3 18.42 5.31 K3 eye 764 19 32 28 69 34.6 +26.7 18.52 4.69 K0 eye 34A 0 46 3 57 33.1 +9.4 18.94 3.44 G0 eye 139 3 17 56 -43 15.6 +86.8 20.25 4.26 G5 eye 66A 1 37 54 -56 26.9 +22.5 21.32 5.07 K0 eye 66B 1 37 54 -56 26.9 +19.4 21.32 5.90 K0 eye 566A 14 49 5 19 18.4 +3.9 22.03 4.54 G8 eye 566B 14 49 5 19 18.4 +5.4 22.03 6.91 K5 892 23 10 52 56 53.5 -17.8 22.18 5.57 K3 eye 33 0 45 45 5 1.4 -12.6 22.62 5.75 K2 eye 105A 2 33 20 6 39.0 +23.4 22.64 5.82 K3 eye, UD 667A 17 15 33 -34 56.2 +1.2 23.29 5.91 K3 eye 667B 17 15 33 -34 56.2 -0.0 23.29 7.20 K5 17 0 17 29 -65 10.1 +8.8 23.44 4.23 G0 eye 68 1 39 47 20 1.6 -33.7 24.32 5.24 K1 eye 178 4 47 7 6 52.5 +24.3 24.70 3.19 F6 eye 673 17 23 16 2 10.2 -28.3 24.70 7.53 K7 666A 17 15 15 -46 35.1 +23.6 24.89 5.48 G8 eye 713 18 21 58 72 42.7 +32.5 25.27 3.58 F7 eye, SB AB 879 22 53 37 -31 49.8 +9.0 25.47 6.49 K5 117 2 50 7 -12 58.3 +18.8 25.67 6.05 K0 23A 11 15 31 31 48.6 -15.5 25.67 3.79 G0 eye, SB AB 423B 11 15 31 31 48.6 -15.9 25.67 4.80 G0 eye, SB 216B 5 42 21 -22 26.2 -10.1 26.50 6.15 K2 216A 5 42 23 -22 27.8 -9.7 26.50 3.60 F6 eye 502 13 9 32 28 7.9 +6.1 27.17 4.26 G0 eye 785 20 12 10 -27 11.0 -54.2 27.17 5.73 K0 eye, SB 506 13 15 47 -18 2.0 -8.5 27.39 4.74 G6 eye 827 21 22 20 -65 35.6 -29.5 28.10 4.22 F6 eye 231 6 11 44 -74 44.2 +34.9 28.35 5.08 G5 eye 75 1 44 6 63 36.4 +1.8 28.59 5.63 K0 eye ========================================================================== Page 54 Table 5 is an extract from the list (provided by the SETI Institute) of the closest stars that form the group of 800 stars which are subject to MOP's "Targeted Search". [40-45] Presently, the list covers stars in the range of 4.39 to 81.5 light years from Earth, but is subject to review. UD = White Dwarf 559A = Alpha Centauri A EB = Eclipsing Binary 144 = Epsilon Eridani AB = Astrometric Binary 71 = Tau Ceti SB = Spectral Binary eye = Visible to the unaided eye under good conditions (apparent visual magnitude less than 6.0 - about 224 stars). The Amateur Optical SETI system just described is quite capable of being upgraded in sensitivity by slaving "n" similar telescopes together, and combining the photons from the "n" optical fibers through a single monochromator and photon-counter. In this way, ten telescopes of 25-cm (10") aperture would have approximately the same sensitivity as a single 81-cm (32") telescope, but in a more cost-effective manner. Of course, ten small telescopes would not have the same ability as a 32" (81 cm) telescope to reject the effects of daylight, should daylight Optical SETI be desired. The approach could be adopted, as with the original Cyclops Study, to gradually increase the number of telescopes as the need arises and availability of funding, assuming that ETI signals are not detected soon after system activation. A large, single barrel, telescope could be constructed using several smaller mirrors, each with its own focus and optical fiber. In this way, only one drive system would be required. A much simpler construction is possible because we do not need to image a star field, just collect as many photons as possible from the region around a single star (light-bucket mode of operation). This could be somewhat like the Multi-Telescope Telescope (MTT) that has been designed by Georgia State University's (GSU) Center for High Angular Resolution Astronomy (CHARA). [92] LIST OF PREVIOUS AND PRESENT OPTICAL SETI ACTIVITIES The following material has been extracted from a comprehensive list on all modern-day SETI activities so far, and was prepared in October of 1991 by Dr. Jill Tarter of the SETI Institute. Dr. Tarter lists sixty three different SETI observing programs, starting with Project Ozma in 1960 at the Green Bank National Radio Observatory in West Virginia, to Harvard University's microwave search of Messier M31 and M33 from the Oak Ridge Observatory. This list also includes the 1983-1984 Amateur Microwave SETI program organized by Dr. Kent Cullers, which used Silicon Valley Hams with their satellite TV dishes (TVROs). Of this list of sixty three observing programs, only three were or are concerned with Optical SETI, and these optical programs are listed Page 55 below. Optical SETI observing programs currently amount to less than 5 percent of all SETI programs to date. In actuality, the ratio is nearer 3 percent because Shvartsman's two programs can be considered as one. This supports the author's contention that Optical SETI has suffered benign neglect. Date: 1973 - 1974 Observer(s): Shvartsman et al. "MANIA" Site: Special Astrophysical Observatory (former Soviet Union) Instrument Size (m): 0.6 Search Wavelength (nm): 550 Frequency Resolution (Hz): df = 100 kHz (dWl = 10^-7 nm) Objects: 21 Peculiar Objects Reference: 48 Comments: Optical search for short pulses of length 3 X 10^-7 to 300 seconds, and narrow laser lines. Prototype for later system on 6 m telescope. Date: 1978 to Present Observer(s): Shvartsman et al. "MANIA" Site: Special Astrophysical Observatory (former Soviet Union) Instrument Size (m): 6 Search Wavelength (nm): 550 Frequency Resolution (Hz): df = 100 kHz (dWl = 10^-7 nm) Objects: 93 Objects Flux Limits: < 3 X 10^-4 of the optical flux is variable in any object observed. Total Hours: 250 Reference: 54 and 58 Comments: Have searched 30 Radio Objects with Continuous Optical Spectra to date, looking for optical pulses from potential Kardashev type II or III civilizations. Date: 1990 to Present Observer(s): Betz Site: Mt. Wilson Instrument Size (m): 1.65 m element of Townes IR Interferometer Search Wavelength (um): 10.6 Frequency Resolution (Hz): 3.5 MHz (35 m/s) Objects: 100 nearby solar-type stars Flux Limits: 1 MW transmitter out to 20 psc Total Hours: Continuing Reference: 57 Comments: Search for IR beacons at CO2 laser frequency using narrowband acousto- optical spectrometer. Continued
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