Patent Publication Number: US-6711912-B2

Title: Cryogenic devices

Description:
CROSS REFERENCE TO RELATED APPLICATIONS 
     This application is a continuation-in-part of U.S. Ser. No. 09/948,498, filed on Sep. 7, 2001, now ABN which claims priority under 35 U.S.C. §119 from U.S. Provisional Appln. Ser. No. 60/230,682, filed Sep. 7, 2000, and U.S. Provisional Appln. Ser. No. 60/265,917, filed Feb. 2, 2001, all of which are incorporated by reference herein as if fully set forth. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     This invention relates generally to cryogenic front-end receivers and, more particularly, to cryogenic front-end receivers of minimal size based on super-conducting elements, low thermal transmission interconnects, self-resonating filters and low dissipated power profile. 
     2. Description of the Related Art 
     Until the late 1980s, the phenomenon of superconductivity found very little practical application due to the need to operate at temperatures in the range of liquid helium. In the late 1980s ceramic metal oxide compounds containing rare earth elements began to radically alter this situation. Prominent examples of such materials include YBCO (yttrium-barium-copper oxides, see WO88/05029 and EP-A-0281753), TBCCO (thallium-barium-calcium-copper oxides, see U.S. Pat. No. 4,962,083) and TPSCCO (thallium-lead-strontium-calcium-copper oxides, see U.S. Pat. No. 5,017,554). All of the above publications are incorporated by reference for all purposes as if fully set forth herein. 
     These compounds, referred to as HTS (high temperature superconductor) materials, exhibit superconductive properties at temperatures sufficiently high enough to permit the use of liquid nitrogen as a coolant. Because liquid nitrogen at 77K (196° C./321° F.) cools twenty times more effectively than liquid helium and is ten times less expensive, a wide variety of potential applications began to hold the promise of economic feasibility. For example, HTS materials have been used in applications ranging from diagnostic medical equipment to particle accelerators. 
     Currently one of the fastest growing applications for superconductivity lies in the area of electronics and associated microwave engineering, due to the astronomical growth in the telecommunications industry and the increased use of consumer electronics by the general population. In spite of the recent advances in superconductivity, however, size, cost and power requirements have limited the commercial use of this promising technology in all but high-end applications such as space instrumentation and military applications. 
     An essential component of many electronic devices, and particularly in the communications field, is the filter element. HTS filters have significant advantages in extremely low in-band insertion loss, high off-band rejection and steep skirts due to the extremely low radio frequency (RF) loss in the HTS materials. 
     However, the conventional transmission line HTS filters, having conventional HTS resonators (such as strip line resonators) as building blocks, require a large substrate area due to the area requirement that at least one dimension of the resonator be equal to approximately half a wavelength (i.e. λ/2). See, for example, U.S. Pat. No. 5,616,538 (incorporated by reference for all purposes as if fully set forth herein). Thus, in conventional low frequency HTS filters having multiple poles and coupled with conventional semiconductor electronic components, such as gallium arsenide (GaAs) amplifiers, the cryogenic coolers required to cool the HTS materials to below their critical temperature (T c ) are relatively large and require heat lifts of at least 6 watts at 80K at an ambient temperature of 20° C. 
     FIG. 1 is a perspective view of such a conventional prior art cryogenic receiver. The overall integrated package consists of several distinct elements. The connectors  110  are used for bringing power and RF signals in and out of the cryoelectronic section, which consists of a dewar assembly  120  containing cryoelectronic components  130  such as RF filters and amplifiers. The dewar assembly  120  is the vacuum cavity necessary to reduce convective heat loading to the cryoelectronic components from molecules within the dewar assembly  120 . A cryogenic source, in this case a cooler  140 , provides the cooling for the cryoelectronic section. The enclosure  150  is an outer package containing the previously described elements as well as circuit boards  160  which provide control functions for the cooler and other error or failure detection and alarms, and a fan  170  for cooling the circuit boards  160 . 
     The size of a conventional unit, as illustrated in FIG. 1, is typically on the order of at least about 15 inches wide×20 inches long×10 inches deep (about 38.1×50.8×25.4 cm). The large size and weight of these conventional units stems predominately from the cooling required due to the physical size of the cryoelectronic section, the power required for the amplifiers, and additional convective heat flow from the RF transitions (normally coaxial cables with connectors), from ambient conditions into the dewar assembly  120 . The physical size, weight and total operating power supplied to the unit is thus dominated by the cooler  140  and dewar assembly  120 . For the conventional unit, the cooling lift required per channel is about 1W when operated at 20° C., thus the total operational power needed for the cooler  140  alone is &gt;125W. 
     Examples of conventional units are the Superfilter™ Systems available from Superconductor Technologies Inc., Santa Barbara, Calif. (see www.suptech.com for more information), and the ClearSite™ systems available from Conductus Inc., Sunnyvale, Calif. USA (see www.conductus.com for more information). 
     The large size and weight of these conventional units substantially limits the application of this technology. One such application is a tower top application in which a receiver front-end is mounted onto an antenna of a cellular or similar base station, such as those disclosed in U.S. Pat. No. 6,104,934 (incorporated by reference for all purposes as if fully set forth herein). The size and cooling requirements of the disclosed receiver are such that the cooling unit must be placed somewhere adjacent the antenna, and is not combinable with the electronics into an integrated unit. 
     For miniaturization purposes, the components comprising the greatest real estate needed are the cooler  140 , cryoelectronic components  130  and dewar assembly  120 . 
     One way to reduce the real estate requirements of a cryoelectronic front-end receiver is to employ lumped element architecture based on conventional HTS filters. These filters can be made to operate at frequencies below 5 GHz with a somewhat more compact physical size; however, filter performance of these conventional lumped element HTS filters is generally limited by intermodulation products and insertion loss. 
     The use of devices containing HTS filters presents other design problems. For example, the interconnects typically utilized to connect the cryogenic portion of the device (usually a dewar containing the HTS filter under vacuum) to other electronic components are long coaxial cables. These long cables, because of their length, exhibit low thermal transmission, which is highly desirable in a cryogenic system where keeping components cold is critical. However, these long cable lines also exhibit RF losses, thus contributing to degradation in RF performance (i.e. an increase in the signal-to-noise ratio). To compound problems even further, the long cables also require the dewar of the cryogenic portion of the device to be larger in volume, which requires a design capable of maintaining the vacuum necessary over the life of the unit, which is more difficult to achieve. 
     There has been a long felt need, as well as numerous attempts by persons of ordinary skill in the art, to reduce the size of filter elements constructed of HTS materials. U.S. Pat. No. 6,108,569, incorporated by reference herein for all purposes as if fully set forth, discloses the use of self-resonant spiral resonators to reduce the size of HTS material filters and concurrently solves cross-talk and connection problems. In spite of the great potential for miniaturization afforded by significant recent technological advances, the problems of vacuum degradation, high thermal transmission, and high dissipated power semiconductor devices, have resulted in less than optimum performance and yielded increased cooling costs. 
     Furthermore, conventional cryogenic front-end receivers require substantial time to manually tune the filters comprising a critical function of the unit. Since the resonating filters in a conventional filter construction do not each vary in a lock-stepped fashion, each pole of the filter must be individually tuned and the tuning of each pole affects every other pole in the filter array. The tuning process can typically take days to perform. 
     Moreover, conventional cryogenic front-end receivers also require the outgassing of molecules that adhere to the device walls during the manufacturing process. Typically, this problem is overcome by simply heating the device slowly over an extended period of time to outgas the gases, such as residual oxygen, nitrogen, carbon dioxide, argon, water vapor. The process normally takes days to complete, because the temperatures necessary to outgas the device walls in a short time period would damage the compressor motor comprising part of the cryogenic unit. 
     The prior art lacks a cryogenic front-end receiver of reduced size capable of being employed adjacent to or integrated with a receiver and/or transmitter. 
     The prior art also lacks a cryogenic front-end receiver with interconnections between the dewar and the cryogenic coolers exhibiting an extremely low thermal transmission to further thermally isolate the dewar. 
     The prior art additionally lacks a cryogenic front-end receiver having interconnections employing a thermal break material and a self-tuning reduced length for reducing RF losses and improving degradation in RF performance. 
     The prior art further lacks a cryogenic front-end receiver having reduced power consumption capabilities. 
     The prior art lacks a cryogenic front-end receiver employing reduced substrate size resonating filters made of HTS materials and resonating at frequencies below 5 GHz. 
     The prior art lacks a method for outgassing a vacuum dewar employing differential heating of the dewar assembly. 
     The prior art lacks a cryogenic front-end receiver capable of being tuned by varying the internal operating temperature of the front-end receiver. 
     SUMMARY OF THE INVENTION 
     The present invention has been made in view of the above circumstances and has as an aspect a cryogenic front-end receiver. 
     A further aspect of the present invention can be characterized as a cryogenic device, the device including a cryogenic electronic portion and a non-cryogenic electronic portion further including a thermal break section. 
     To achieve these and other advantages and in accordance with the purpose of the present invention, as embodied and broadly described, the present invention can be characterized, according to one aspect, as a cryogenic front-end unit, the unit including a cryogenic electronic unit, wherein the cryogenic unit includes a input signal interface and output signal interface. A cryogenic cooler is in thermal communication with the cryogenic electronic unit. The cryogenic unit further includes an input signal interconnect that is connected to the input signal interface and an output signal interconnect that is connected to the output signal interface. 
     Another aspect of the present invention can be characterized as a cryogenic device including a cryogenic electronic portion, a non-cryogenic electronic portion and an interconnect connecting the cryogenic and non-cryogenic electronic portions, wherein the interconnect comprises a thermal break between cryogenic and non-cryogenic electronic portions. 
     A further aspect of the present invention can be characterized as a cryogenic device including a cryogenic electronic portion contained within a vacuum dewar assembly, the cryogenic electronic portion having an input end and an output end, and an ambient to cryogenic input connector having an ambient end passing through the vacuum dewar assembly to a cryogenic end connected to the input end of the cryogenic electronic portion. A cryogenic to ambient output connector with a cryogenic end connected to the output end of the cryogenic electronic portion, passes through the vacuum dewar assembly to an ambient end. A cryogenic source is connected to the vacuum dewar assembly so as to be in intimate contact with the cryogenic electronic portion, which has an input end and an output end. The cryogenic electronic portion includes at least one of a high temperature superconductor filter element and a cryogenic active semiconductor circuit (such as a low-noise amplifier). The input end of the cryogenic electronic portion is connected to the cryogenic end of the input connector and the output end of the cryogenic electronic portion is connected to the cryogenic end of the output connector. In the event that an active semiconductor circuit is used, that active semiconductor circuit should produce a total dissipated power into the cryogenic electronic portion of less than about 850 mW. The cryogenic device has a maximum cooler lift of less than about 3 W at 80K at an ambient temperature of 20° C. 
     Stated another way, this aspect of the present invention relates to a cryogenic device comprising: 
     (1) a cryogenic electronic portion contained within a vacuum dewar assembly, the cryogenic electronic portion having an input end and an output end; 
     (2) an ambient to cryogenic input connector having an ambient end passing through the vacuum dewar assembly to a cryogenic end connected to the input end of the cryogenic electronic portion, 
     (3) a cryogenic to ambient output connector having a cryogenic end connected to the output end of the cryogenic electronic portion, passing through the vacuum dewar assembly to an ambient end; and 
     (4) a cryogenic source connected to the vacuum dewar assembly so as to be in intimate contact with the cryogenic electronic portion, 
     wherein: 
     (i) the cryogenic electronic portion comprises at least one of a high temperature superconductor filter element and a cryogenic active semiconductor circuit, 
     (ii) an active semiconductor circuit, if present, produces a total dissipated power into the cryogenic electronic portion of less than about 850 mW, and 
     (iii) the cryogenic device has a maximum cooler lift of less than about 3 W at 80K at an ambient temperature of 20° C. 
     Another aspect of the present invention can be characterized as a cryogenic receiver in which the cryogenic electronic portion of the above-mentioned cryogenic device comprises a high temperature superconductor filter element having an input end and an output end, and an active semiconductor circuit having an input end and an output end, wherein the input end of the active semiconductor circuit is connected to the cryogenic end of the input connector via the high temperature superconductor filter element. The input end of the filter element is connected to the cryogenic end of the input connector and the output end of the filter element is connected to the input end of the active semiconductor circuit. 
     Stated another way, this other aspect relates to a cryogenic receiver in which the cryogenic electronic portion of the above-mentioned cryogenic device comprises a high temperature superconductor filter element having an input end and an output end, and an active semiconductor circuit having an input end and an output end, wherein: 
     the input end of the active semiconductor circuit is connected to the cryogenic end of the input connector via the high temperature superconductor filter element; 
     the input end of the filter element is connected to the cryogenic end of the input connector; and 
     the output end of the filter element is connected to the input end of the active semiconductor circuit. 
     A still further aspect of the present invention can also be characterized as a cryogenic receiver including a cryogenic electronic portion contained within a vacuum dewar assembly, the cryogenic electronic portion having an input end and an output end. An ambient to cryogenic input connector having an ambient end passes through the vacuum dewar assembly to a cryogenic end connected to the input end of the cryogenic electronic portion, and a cryogenic to ambient output connector having a cryogenic end connected to the output end of the cryogenic electronic portion passes through the vacuum dewar assembly to an ambient end. The cryogenic receiver further comprises a cryogenic source connected to the vacuum dewar assembly so as to be in intimate contact with the cryogenic electronic portion. The cryogenic electronic portion additionally includes a high temperature superconductor filter element having an input end and an output end, and an active semiconductor circuit having an input end and an output end. The input end of the filter element is connected to the cryogenic end of the input connector and the output end of the filter element is connected to the input end of the active semiconductor circuit. The output end of the active semiconductor circuit is connected to the cryogenic end of the output connector and the active semiconductor circuit produces a total dissipated power into the cryogenic electronic portion of less than about 850 mW. The cryogenic receiver has a maximum cooler lift of less than about 3 W at 80K at an ambient temperature of 20° C. 
     Stated another way, this still further aspect of the present invention also relates to a cryogenic receiver comprising: 
     (1) a cryogenic electronic portion contained within a vacuum dewar assembly, the cryogenic electronic portion having an input end and an output end; 
     (2) an ambient to cryogenic input connector having an ambient end passing through the vacuum dewar assembly to a cryogenic end connected to the input end of the cryogenic electronic portion, 
     (3) a cryogenic to ambient output connector having a cryogenic end connected to the output end of the cryogenic electronic portion, passing through the vacuum dewar assembly to an ambient end; and 
     (4) a cryogenic source connected to the vacuum dewar assembly so as to be in intimate contact with the cryogenic electronic portion, 
     wherein: 
     (i) the cryogenic electronic portion comprises: 
     (a) a high temperature superconductor filter element having an input end and an output end, and 
     (b) an active semiconductor circuit having an input end and an output end, 
     (ii) the input end of the filter element is connected to the cryogenic end of the input connector, 
     (iii) the output end of the filter element is connected to the input end of the active semiconductor circuit, 
     (iv) the output end of the active semiconductor circuit is connected to the cryogenic end of the output connector, 
     (v) the active semiconductor circuit produces a total dissipated power into the cryogenic electronic portion of less than about 850 mW, and 
     (vi) the cryogenic receiver has a maximum cooler lift of less than about 3 W at 80K at an ambient temperature of 20° C. 
     The reader should note that when one “component” is connected to another “component,” only a sequence is implied and, as such, other components may be connected in between. For example, input connector-filter element-active semiconductor-output connector is a sequence that can be interrupted by other components. It is generally accepted practice to keep the number of components in the vacuum dewar assembly to a minimum (e.g., to reduce cooling requirements), so it is desirable to have a direct connection from the input connector to the filter element, the filter element to the active semiconductor device, and the active semiconductor device to the output connector, as discussed in further detail below. 
     With the combination of the HTS filters (particularly those based on self-resonating spiral resonators), low dissipated power semiconductor devices (that operate effectively under the required cryogenic conditions) and the interconnects as mentioned above, much smaller cryogenic devices (such as low noise receivers) can be constructed and cooled by smaller cryogenic coolers since these devices require cooler lifts of less than about 3 watts, more preferably less than about 2 watts, and still more preferably about 1 watt or less, to cool the cryoelectronic section to 80K at an ambient temperature of 20° C. In other words, the present invention provides miniature cryogenic devices delivering optimum performance at minimal size and cooling cost. 
     An additional benefit to the miniaturization enabled by the present invention is a significant reduction in the heat budget of the operating unit, which has a direct correlation to improved cryocooler efficiency, increased system operational life and reliability, and reduced energy consumption and operating costs. 
     Positioning the active semiconductor device outside the cryogenic electronic portion of the cryogenic device, i.e., placing it in the non-cryogenic electronic portion, further reduces the heat budget of the operating unit. This aspect of the present invention relates to a cryogenic device, e.g., a cryogenic receiver, comprising: 
     (1) a cryogenic electronic portion contained within a vacuum dewar assembly, the cryogenic electronic portion having an input end and an output end; 
     (2) an ambient to cryogenic input connector having an ambient end passing through the vacuum dewar assembly to a cryogenic end connected to the input end of the cryogenic electronic portion, 
     (3) a cryogenic to ambient output connector having a cryogenic end connected to the output end of the cryogenic electronic portion, passing through the vacuum dewar assembly to an ambient end; and 
     (4) a cryogenic source connected to the vacuum dewar assembly so as to be in intimate contact with the cryogenic electronic portion, 
     wherein, the cryogenic electronic portion consists essentially of a high temperature superconductor filter element. The high temperature superconductor filter element may be comprised of one or more mini-filters based on self-resonant spiral resonators. 
     This aspect of the present invention can be further characterized as a cryogenic device or cryogenic receiver in which the high temperature superconductor filter element in the cryogenic electronic portion of the above-mentioned cryogenic device or cryogenic receiver has an input end and an output end, wherein the input end of the high temperature superconductor filter element is connected to the cryogenic end of the input connector and the output end of the high temperature superconductor filter element is connected to the cryogenic end of the output connector. 
     The present invention also provides a method of tuning a cryogenic receiver comprising a high temperature superconducting filter element, said cryogenic receiver being programmed to operate at a specified operating frequency at a specified temperature, comprising the step of altering the specified operating temperature to induce a shift in the operating frequency of the cryogenic receiver. 
     The present invention also provides a method for outgassing the vacuum dewar assembly of a cryogenic device comprised of the vacuum dewar assembly and a cryocooler in close proximity, comprising: 
     (a) pumping on the vacuum dewar assembly with a vacuum pump; 
     (b) contacting the cryocooler with a heat sink capable of maintaining the cryocooler at a sufficiently low temperature to avoid damage to the cryocooler; and 
     (c) raising the temperature of the vacuum dewar assembly to increase outgassing. 
     The present invention also provides a method for activating a getter used in the vacuum dewar assembly of a cryogenic device comprised of the vacuum dewar assembly and a cryocooler in close proximity, wherein the getter is contained in integral appendages of the dewar body of the vacuum dewar assembly, comprising: 
     (a) pumping on the vacuum dewar assembly with a vacuum pump; and 
     (b) raising the temperature of the appendages by means of an external heater to a temperature sufficient to activate the getter. 
     This invention also provides a communications tower having an integrated antenna assembly located at the top of the tower, and a telecommunications network utilizing such a communications tower. 
     These and other features and advantages of the present invention will be more readily understood by those of ordinary skill in the art from the following detailed description. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed. For example, it is to be appreciated that certain features of the invention which are, for clarity, described below in the context of separate embodiments, may also be provided in combination in a single embodiment. Conversely, various features of the invention which are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombination. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate several embodiments of the invention and together with the description, serve to explain the principles on of the invention. 
     FIG. 1 shows a perspective view of a conventional integrated cryogenic receiver; 
     FIG. 2 shows a front tilt perspective view of an embodiment of a cryogenic receiver in accordance with the present invention; 
     FIG. 2A shows a top perspective view of an embodiment of a cryogenic receiver in accordance with the present invention; 
     FIG. 3 is a diagram of a microstrip transmission line with a thermal break that can be used as part of an ambient to cryogenic (or vice versa) connector; 
     FIG. 4 is a diagram of a waveguide structure with a thermal break that can also be used as part of an ambient to cryogenic (or vice versa) connector; 
     FIG. 5A shows a front-tilted perspective view of a hermetically sealed cryogenic receiver of an embodiment of the present invention; 
     FIG. 5B shows front-tilted exploded perspective view of the embodiment shown in FIG. 5A of the present invention; 
     FIG. 5C is an expanded front-tilted perspective view of the embodiment shown in FIG. 5B of those elements above cut line  5 C— 5 C of the present invention; 
     FIG. 5D is an expanded front-tilted perspective view of the embodiment shown in FIG. 5B of those elements above cut line  5 D— 5 D and below cut line  5 C— 5 C of the present invention; 
     FIG. 5E is an expanded front-tilted perspective view of the embodiment shown in FIG. 5B of those elements below cut line  5 D— 5 D of the present invention; 
     FIG. 6A depicts a schematic circuit diagram of a cryogenic receiver including a main antenna and a diversity receiver antenna input configuration of an embodiment of the present invention; 
     FIG. 6B depicts a schematic circuit diagram of a cryogenic receiver including a main antenna and a diversity receiver antenna input configuration with multiple receiver inputs and a bypass circuit configuration of an alternate embodiment of the present invention; 
     FIG. 6C depicts a schematic circuit of a cryogenic receiver including a transmit antenna and a receive antenna input including a bypass circuit and filter configuration of an alternate embodiment of the present invention; 
     FIG. 6D depicts a schematic circuit diagram of a cryogenic receiver including a main antenna input, a bypass circuit configuration and no active semiconductor circuit, i.e., amplifier, in the cryogenic unit, of an alternate embodiment of the present invention; and 
     FIG. 6E depicts a schematic circuit of a cryogenic receiver including a main antenna input with multiple diplexers, a bypass circuit configuration and no active semiconductor circuit, i.e., amplifier, in the cryogenic unit of an alternate embodiment of the present invention. 
     FIG. 6F depicts a schematic circuit of a cryogenic receiver identical to that shown in FIG. 6C except that there is no active semiconductor circuit, i.e., amplifier, in the cryogenic unit. 
     FIG. 7 depicts a schematic drawing of a cryogenic receiver with a getter appendage that is an integral part of the vacuum dewar assembly. 
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     Reference will now be made in detail to the present embodiments of the present invention, and examples of which are illustrated in the accompanying drawings. Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts (elements). 
     The present invention overcomes the deficiencies of the prior art as stated above and provides technical advantages over the prior art in the areas of receiver size, power requirement, thermal isolation, integration with a receiver or transmitter and interconnections of reduced length for reducing RF losses. 
     It should be noted that the word “ambient”, as used herein, refers to conditions present in the surrounding environment, that is, external to the dewar assembly. Ambient can, for example, refer to normal room conditions, elevated temperature conditions present as a result of a warm day and/or heat generated in the operation of the equipment, or low temperature conditions existing in outer space. This is opposed to “cryogenic” which refers to conditions within the dewar assembly, that is, an environment that is purposefully cooled (with a cryogenic source) to maintain a desired low temperature for optimal operation of the cryogenic electronic portion. 
     An improvement in the current state of the art, in accordance with the present invention, is shown in FIGS. 2,  2 A and  5 A- 5 E. Depicted is a cryogenic receiver in which the cryogenic electronic portion is, for illustration purposes, a combination of an HTS filter element  205  connected to an active semiconductor circuit  210 , and contained in a vacuum dewar assembly  215 . The vacuum dewar assembly  215  comprises a body  220  and, as a base, bottom plate  565 . A cold plate  225  is in intimate contact or in close proximity to both the cryogenic electronic portion and a cryogenic source. In this embodiment the cryogenic source is a miniature cryocooler  230 . The vacuum dewar assembly  215  is a self-contained unit comprising a housing or enclosure. Vacuum dewar assembly  215  includes a cover or lid  520 , as shown in FIG.  5 A. Generally speaking, the vacuum dewar assembly  215  and cryocooler  230  are in close proximity to one another. In an alternate embodiment, vacuum dewar assembly  215  and cryocooler  230  are in close proximity with each other or formed as an integral unit or assembly (affixed to one another) as depicted in FIG. 2 
     The vacuum dewar assembly  215  may also contain, for example, a thermal/infrared heat shield  235  covering at least the HTS filter element  205 , to further reduce the cooling and power requirements of the cryogenic device. 
     In another embodiment the size of the cryogenic device can be further reduced by placing a superconducting plate (not depicted) on the underside of thermal/infrared heat shield  235  facing at least the HTS filter element  205  and further in intimate contact with cold plate  225 . The application of the superconducting plate in the present embodiment assists in providing reduced surface area for the cryogenic device element and thus further reduce the cooling and power requirements of the device. 
     The superconducting plate can comprise, for example, a disk with a film of an HTS material on at least the side of the disk facing the HTS filter element  205 . The disk typically is not in physical contact with the HTS filter element  205 , but can be as close to HTS filter element  205  without contact as the construction of the dewar assembly allows. In order to be in contact with cold plate  225  but not HTS filter element  205 , the disk can contain one or more spacer legs or edges. Generally, the disk covers as much of the cryogenic electronic portion as the construction of the dewar assembly allows. 
     The superconducting plate can also be used for tuning purposes such as, for example, disclosed in U.S. application Ser. No. 09/727,009 (filed Nov. 30, 2000) (corresponding to WO01/41251), which is incorporated by reference for all purposes as if fully set forth herein. 
     A method that can be used for tuning is to modify the temperature at which the unit is programmed to operate. For instance, the difference in temperature in a unit operating at 79.5K versus 80.0K can, depending on filter design, introduce a shift in the operating frequency of the HTS filter element  205  of up to 200 kHz. This temperature adjustment can be made by varying the set point temperature of the temperature controller for the cryocooler  230 . Another way of adjusting this temperature is to modify the temperature voltage curve of a temperature measurement silicon diode or Resistive Temperature Device (RTD) in the controller or adding an additional resistance in series with the RTD or silicon diode and leaving the voltage curve fixed. 
     In an alternate embodiment the operating temperature of the cryogenic unit can be varied such that the unit could operate at a second center frequency for emergency or back-up purposes in narrow band applications. For instance, if a unit is designed to operate at 1950 MHz center point frequency with a bandwidth of 2 MHz, the operational range would be 1949-1951 MHz. By varying the operating temperature, the unit can be made to operate at center point frequency of 1949 MHz with a bandwidth ranging from 1948-1950 MHz. The temperature can also be varied in smaller increments to fine tune the cryogenic unit, wherein the unit is operating slightly off center of its intended center point frequency due to variations in the manufacturing process. 
     The cryogenic electronic portion is connected to input sources and output components, as illustrated in FIGS. 2,  2 A and  5 A, through, respectively, input and output connectors  240  and  245 , which transition from cryogenic conditions within the vacuum dewar assembly  215  to ambient conditions outside the vacuum dewar assembly  215 . 
     As indicated above, the total cooling power required by the cryogenic electronic portion directly affects the size, weight and total operating power of a cryocooler functioning as the cryogenic source. The larger the total cooling power required, the larger the size, weight and total operating power of the cooler. The total cooling power required is a function of a number of factors including, but not limited to, the infrared heating of the cold surfaces, conductive heat flow by gas molecules from warm surfaces to the cold surfaces, the power dissipated by the active semiconductor circuit  210  into the vacuum dewar assembly  215 , and the conductive heat leak due to the connectors  240  and  245  and the jumpers  250  and  255 . Infrared heating of the cold surfaces can be reduced by altering the size of the cold surfaces and the temperature at which the cold surfaces are held relative to ambient. The size of the cold surfaces is determined primarily by filter size and packaging. 
     In addition to the features detailed above, the present invention, as depicted in FIGS. 2 and 2A, employs a number of other features to reduce the size and total cooling power required to maintain the cryogenic electronic portion at an optimal operating temperature. 
     As can be seen from FIGS. 2 and 2A, the connectors  240  and  245  are made integral to the vacuum dewar assembly  215  as opposed to a separate module  110  as depicted in Prior Art FIG.  1 . The jumpers  250  and  255  are connected, respectively, to input and output hermetic connectors  240  and  245 . The hermetic connectors  240  and  245  provide the electrical transition into and out of the vacuum dewar assembly  215  and utilize, for example, “O”-rings, soldered seals and/or direct glass to metal seals to maintain the vacuum seal within the vacuum dewar assembly  215 . Direct glass to metal seals generally provide a suspension seal. The portion of hermetic connectors  240  and  245  outside of the dewar assembly can, for example, be in the form of coaxial or other well-known connectors, such as fiber-optics, twisted pairs and the like, depending on the type of connection required. To use a fiber optic connection would require conversion of the RF signal to an encoded light signal. 
     Jumpers  250  and  255  transition from cryogenic temperatures at the connections to the cryogenic components to ambient temperatures at the connections to the hermetic connectors  240  and  245 . The jumpers  250  and  255  can be of conventional construction, depending on the end use, for example, a microstrip transmission line for lower frequency signals or a waveguide for higher frequency signals. In an alternate embodiment the interconnects (i.e. jumpers  250  and  255 ) are formed on a thermal break material to reduce thermal gain from the ambient. For example, jumpers  250  and  255  can be formed as a microstrip transmission line on a substrate such as alumina, glass (fused silica, quartz or MACOR), fiberglass epoxy, or aerogel whose thickness is &gt;0.002 inches (&gt;0.051 mm). The substrates for the jumpers utilized in the present invention are constructed of very low thermal conductive materials that function as effective thermal breaks, such as fused silica (thermal conductivity (K) of about 1.5 W/m-K) or silica-based aerogels (K values of from about 0.02 W/m-K (300K, 1 atmosphere) to 0.004 W/m-K (300K, vacuum)). In an alternate embodiment higher thermal conductivity substrates are contemplated that also include a thermal break material of some type. Skilled artisans will appreciate that numerous thermal breaks may be employed and not depart from the teachings of the present invention. 
     An example of this embodiment is depicted in FIG. 3, wherein an interconnect includes an inserted thermal break. Substrate material  310  contains an insert  320  of a low thermal conductivity material (such as aerogel) between the colder end  330  and warmer end  340  of the conductive strip  350  on the microstrip line. In a similar context, a waveguide cavity can be constructed of a low thermal conductive material such as aerogel that is metallized on at least the interior surface, or can be constructed of a standard material such as a metal with an inserted thermal break. An embodiment of the inserted thermal break material in a metallic waveguide is depicted in FIG. 4, where substrate material  310  contains an insert  320  of a low thermal conductive material (such as aerogel), metallized on at least the interior surface  410 , between the colder end  330  and warmer end  340  of the waveguide cavity. 
     It should be noted that, while thermal breaks additionally reduce thermal conductivity from the ambient, low thermal conductivity materials should be utilized as the primary means to avoid as much conductive heat gain in the cryogenic electronic portion as possible. A combination of low thermal conductivity materials and well as the application of a thermal breaks in the design generally provides the best of both, but at a cost of increased size and thus may not be practical in all applications. 
     Because conductive heat flow is inversely proportional to the length of the conductive material, jumpers  250  and  255  (see FIG. 5D) can be lengthened, although this may lead to increased signal losses and an increase in the size of the vacuum dewar assembly. The trade off between RF loss and lower thermal gain, however, can be optimized by the person of ordinary skill in the art based on the materials and dimensions of construction of the jumpers  250  and  255 . 
     A detailed description of the cryogenic receiver as set forth below is made with references to FIGS. 5A-5E. 
     FIG. 5A depicts a front-tilted perspective view of the hermetically sealed cryogenic receiver of the present invention and FIG. 5B depicts a front tilted exploded perspective of FIG.  5 A. The assembly of the cryogenic receiver is as described below with reference to FIGS. 5A-5E, respectively. 
     The lid  520  of the vacuum dewar assembly  215  is capable of being attached to the dewar body  220  by welding, soldering or mechanical connection. As shown in FIG. 5B, screws  522  are inserted through holes in lid  520  and engage body  220  via screw holes  523 . An “O-ring” seal  530  is placed in groove  222  and forms a seal when lid  520  is engaged via screws  522  with body  220 . 
     The O-ring seal  530  is capable of being made of, but is not limited to, rubber, a synthetic material or metal as required to maintain the vacuum conditions. In an alternate embodiment, the attachment of the lid  520  is accomplished by soldering, and O-ring seal  530  is typically made of metal. In a further embodiment of the present invention, wherein some of the components are heat sensitive, thereby rendering conventional welding or soldering techniques difficult to utilize, a “cold” welding technique is capable of being employed in which a malleable metal O-ring (such as one constructed of indium) is placed between the lid  520  and dewar body  220 , and the seal is formed by application of pressure to lid  520  to compress the O-ring  530  into groove  222 . 
     It is important when evacuating a dewar to outgas, i.e., to remove gases that may be adsorbed onto the surfaces of the dewar cavity, e.g.,  555 , being evacuated and adsorbed onto the surfaces of the contents of the dewar cavity. This can be accomplished by pumping on the dewar for a very long time with a vacuum pump. Heating the vacuum dewar assembly during the pumping can greatly accelerate outgassing. However, in a cryogenic device where the vacuum dewar assembly and the cryocooler are in such close proximity that heating the vacuum dewar assembly could damage the cryocooler, for example when they are formed as an integral unit or assembly, the outgassing process takes days to complete because the temperatures necessary to outgas the surfaces of the dewar cavity and of its contents in a short time period must be kept low enough to avoid damage to the compressor motor comprising part of the cryogenic unit. 
     This long outgassing process can be greatly shortened by using a differential heating method in which the vacuum dewar assembly is raised to a higher temperature by means of an external heater to speed the outgassing while the cryocooler is maintained at a lower temperature chosen to avoid damage to the cryocooler. The higher temperature to which the vacuum dewar assembly is raised is chosen so as to avoid damage to the vacuum dewar assembly. Preferably, the heater used to raise the temperature of the vacuum dewar assembly is specifically designed to heat the vacuum dewar assembly, e.g., to fit around or encompass the vacuum dewar assembly  215 , and thereby localize the heating. A heat sink contacting the cryocooler  230  to maintain the temperature at a lower temperature to avoid damage to the cryocooler will preferably surround the cryocooler. For the cryogenic receiver shown in FIGS. 2 and 5, a cylinderical heat sink fitting around cryocooler  230  is an appropriate form for the heat sink. Even small increases in the temperature of the vacuum dewar assembly during outgassing decreases the time appreciably. For instance, with a heater surrounding the vacuum dewar assembly  215  operating at 120° C., the temperature of the cold plate  225  in the vacuum dewar assembly is 70° C. and the outgassing can be accomplished in about 48 hours as compared with many days if carried out with no heating. During this outgassing the cryocooler  230  was maintained at 35° C. With higher vacuum dewar assembly temperatures, the outgassing can be carried out in even faster times. To effect an appreciable decrease in outgassing time, the internal temperature of the vacuum dewar assembly, i.e., the temperature measured at a surface of the dewar cavity being evacuated or at a surface of its contents, should be greater than ambient temperature, i.e. about 20° C. Decreases in outgassing times will be more appreciable if the temperature measured at a surface of the dewar cavity being evacuated or at a surface of its contents is preferably 50° C. or higher, more preferably 70° C. or higher and most preferably 100° C. or higher. The temperature used must not impair any portion of the vacuum dewar assembly. 
     Getter  525 , which absorbs gases left behind once the dewar body  220  has been evacuated via vacuum tube  266 , is held in place by fastener  526  which engages base  527 . In this embodiment there are four getters  525  as illustrated, but any number may be used as long as the getter has sufficient capacity to absorb the expected impurities encumbered over the life of the cryogenic unit. 
     Getters generally are activated by heating to remove any oxide coatings. This heating can be accomplished by passing an electrical current through internal heaters. This activation is carried out before the vacuum tube  266  is sealed. An alternate way to provide for a getter is to have the getter contained in one or more appendages which are an integral part of the vacuum dewar assembly  215 , i.e., an integral part of dewar body  220 , lid  520  or bottom plate  565 . FIG. 7 depicts one such appendage  710  that is an integral part of vacuum dewar assembly  215  and the getter  720  contained in the appendage  710 . The appendage  710  can then be heated to a temperature sufficient to activate the getter  720  contained in the appendage by means of an external heater designed to fit around or encompass the appendage. This eliminates the need to provide means to pass a current through an internal heater. The appendage  710  can be in the form of a hollow cylinder or any other convenient shape and is typically welded to the vacuum dewar assembly  215 . The interior of the appendage becomes an extension of the dewar cavity  555 . Depending on the locations of the one or more appendages and the design of the cryogenic device, the remainder of the vacuum dewar assembly  215  may have to be in contact with a heat sink to maintain the temperature at a level that avoids damage to the vacuum dewar assembly. Depending on the temperature at which the vacuum dewar assembly is maintained, the cryocooler  230  may require contact with a heat sink to maintain its temperature at a lower level. When such appendages are used to contain the getter, external heating can be used to both outgas the surfaces in the dewar cavity as well as to activate the getter. 
     Cold plate  225  is housed within the internal cavity area  555  formed within body  220 . Alignment tool  510  is utilized to align cold plate  225  with the body  220  of the unit. Tool  510  is removed once cold plate  225  is adequately secured within cavity  555 . Filter  205  and active semiconductor circuit (such as an amplifier)  210  are placed on cold plate  225  or in close proximity to cold plate  225 . RF shield (or thermal/infrared heat shield)  235  is placed in communication with cold plate  225  and shields filter  205  and amplifier  210 . Brackets  535 ,  539  and  541  are utilized to hold cold plate  225 , filter  205  and amplifier  210  (i.e. front-end receiver) in their respective positions within cavity  555 . All cryogenic and non-cryogenic surfaces inside the cavity  555  are preferably plated with a highly reflective material such as, for example, gold, platinum, silver or similar type metal (i.e., highly conductive metal with low reactivity to the environment). Jumpers  250  and  255  are in communication with filter  205  and amplifier  210 . 
     Various inputs and outputs are made accessible to the receiver via port  240  (RF in ),  245  (RF out ) and  270  (DC in ). Temperature indication inside of the unit is provided via port  564 . Inputs for controlling the cryocooler are made accessible through port  275 . 
     Cold finger  572  extends through central opening  554  of cavity  555  and is in thermal communication with cold plate  225 . Cold finger  572  extends from the top  280  of cryocooler  230  (i.e. heat sink region). O-ring  570  forms a seal with top  280  when bottom plate  565  is secured via bolts or screws to bolt or screw holes  290  formed in cryocooler top portion  280 . 
     As an example of taking a number of heat budget factors into consideration, by keeping the HTS filter element &lt;40 cm 2  in size, the active semiconductor circuit &lt;350 mW dissipated power, and the thermal leak produced by the jumpers (a microstrip transmission line on a 5 cm long, 0.005″ (0.127 mm) thick, and 5 mm wide fused silica substrate) to &lt;100 mW, one can reduce the cooling capacity required per channel to &lt;600 mW at 80K at 20° C. ambient temperature. 
     As indicated previously, the heat budget can be reduced by positioning the active semiconductor circuit in the non-cryogenic electronic portion of the cryogenic device. In this aspect of the invention the cryogenic electronic portion consists essentially of a high temperature superconductor filter element. Portions of the ambient to cryogenic input connector and the cryogenic to ambient output connector are within the vacuum dewar assembly. The cryogenic ends of these connectors are connected to the high temperature superconductor filter element, i.e., the input end of the high temperature superconductor filter element is connected to the cryogenic end of the input connector and the output end of the high temperature superconductor filter element is connected to the cryogenic end of the output connector. Preferably, the high temperature superconductor filter element is comprised of self-resonant spiral resonators. Moving the active semiconductor circuit out of the cryogenic electronic portion eliminates a major source of heating in the cryogenic electronic portion and facilitates the use of smaller cryogenic coolers since this device requires cooler lifts less than about 3 watts of power, more preferably less than about 2 watts, and still more preferably about 1 watt or less, to cool the cryoelectronic section to 80K at an ambient temperature of 20° C. Embodiments of the invention in which there are no active semiconductor circuits inside the cryogenic unit are represented in FIGS. 6D,  6 E and  6 F. 
     As indicated previously, jumpers  250  and  255  are preferably a microstrip transmission line formed on a fused silica or silica aerogel substrate, which are very low thermal conducting substrates and can effectively be used in a long life vacuum environment due to their absence of outgassing materials which could degrade the vacuum over time and increase the heat load to the cooler due to thermal conduction by the outgassed materials. Additionally, an added benefit to an aerogel substrate is that the material is essentially a large surface area silica material. Silica surfaces tend to absorb water vapor, thus improving the quality of the vacuum. Silica materials such as fused silica or silica aerogel are optimum electrical and thermal interfaces and act as a “getter” helping to maintain the required vacuum in the dewar and thus improving vacuum reliability. 
     In an alternate embodiment, jumpers  250  and  255  comprise a microstrip transmission line (such as a 1.5 μm thick gold line) deposited on one side of a fused silica substrate which is typically 5 cm long, 2.5-5 mm wide and 0.005 inches (0.127 mm) thick, with the other side of the substrate having a grounding layer (e.g., a conductive metal such as gold) thereon. 
     Conventional waveguide cavities made entirely out of conductive metals tend to produce too large a thermal leak to the cryogenic electronic portion for applications in the frequency range of less than approximately 2 GHz. Thus, it is recommended (when a waveguide is applicable) to construct the waveguide cavity from a metal coated substrate having a low thermal conductivity (e.g., aerogel) or, at a minimum, to insert a “thermal break” of metal coated aerogel material into the waveguide cavity structure to reduce the conductive thermal transfer. 
     The HTS filter element may be one or more mini-filter(s) capable of meeting the size limitations imposed by the configuration of the vacuum dewar assembly. Preferred mini-filters are disclosed in previously incorporated U.S. Pat. No. 6,108,569, and are based on self-resonant spiral resonators of varying shapes, including but not limited to rectangular, rectangular with rounded corners, polygon, hairpin, oval and circular. The size of the self-resonant spiral resonator is reduced by reducing the width of the gap between adjacent lines and reducing the center open area in the spiral resonator. The resonant frequency (f) of the self-resonant spiral resonator can be changed by changing the length of the spiral line (λ) (wherein f≈λ/2), changing the gap width between the adjacent lines of the spiral and by placing a conductive tuning pad at the center of the spiral. The last method can be used as fine frequency tuning. Frequency tuning can also be accomplished through the use of an HTS plate positioned above the filter element, and operating temperature variations, as discussed above. 
     The design of the HTS filter element further depends on a number of factors such as, for example, the purpose of the filter element (e.g., band pass or band reject), operating frequency, sensitivity and other factors recognizable by those of ordinary skill in the art. Based on these factors, one of ordinary skill in the art can design an appropriate filter element using the guidance provided in previously incorporated U.S. Pat. No. 6,108,569 and standard design tools such as commercially available software packages (for example, Sonnet EM Suite available from Sonnet Software, Inc.). 
     In various embodiments, the superconducting materials of the HTS filter element (and other components comprising superconducting materials) have a transition temperature, T c , greater than about 77K. In addition, substrates for the HTS filter element should have a dielectric material lattice matched to the HTS film deposited thereon, with a loss tangent less than about 0.0001. Specific preferred materials include (but are not limited to) the following: HTS materials—one or more of YBa 2 Cu 3 O 7 , Tl 2 Ba 2 CaCu 2 O 8 , TlBa 2 Ca 2 Cu 3 O 9 , (TlPb)Sr 2 CaCu 2 O 7  and (TlPb)Sr 2 Ca 2 Cu 3 O 9 ; and substrate materials—one or more of LaAlO 3 , MgO, LiNbO 3 , sapphire and quartz. 
     In addition to the substrate and HTS materials, various buffer and orientation layers can be utilized where appropriate, such as (for example) disclosed in U.S. Pat. No. 5,508,255 and U.S. Pat. No. 5,262,394, both of which are incorporated herein for all purposes as if fully set forth. 
     The input and output couplings of the spiral resonator-based mini-filter have two generally accepted configurations. One is a parallel line configuration, which comprises a transmission line with one end connected to the mini-filter&#39;s connector via a normal metal contact pad on top of the line, the other end of the line being extended to be close by and in parallel alignment with the spiral line of the first resonator (for the input circuit) or the last resonator (for the output circuit) to provide the input or output couplings for the filter. The other is an inserted line configuration, which comprises a transmission line with one end connected to the mini-filter&#39;s connector via a normal metal contact pad on top of the line, with the other end of the line being extended to be inserted into the split spiral line of the first resonator (for the input circuit) or the last resonator (for the input circuit) to provide the input or output couplings for the filter. Further details can be found by reference to previously incorporated U.S. Pat. No. 6,108,569. 
     The inter-resonator couplings between adjacent spiral resonators in the mini-filter are provided by the overlapping of the electromagnetic fields at the edges of the adjacent resonators. The coupling strength can be adjusted by changing the longitudinal distance between adjacent spiral resonators, changing the orientation of the spiral resonators and shifting the spiral resonator&#39;s location along the transverse direction. The last way can be used for fine adjustment of the coupling strength. Again, further details can be found by reference to previously incorporated U.S. Pat. No. 6,108,569. 
     The mini-filter is preferably in intimate contact with the cold plate  225  of the vacuum dewar assembly  215  via a metallized ground plane on the “back” side of the mini-filter substrate, further details of which can be seen by reference to previously incorporated U.S. Pat. No. 6,108,569. The mini-filter and active semiconductor circuit  210  can be affixed to the cold plate  225 , for example, by using conductive epoxy or solder between the metallized ground plane and the cold plate  225 , or by resistive welding of the metallized ground plane to the cold plate  225 , or simply by mechanical means such as screws. 
     The active semiconductor circuit  210  may be connected to the filter element  205  by any conventional means such as soldering, wire bonding or parallel gap welding, but is typically connected by a short metal wire which is attached by solder, thermal compression bonding or resistive welding from contact pads (not shown) on the active semiconductor circuit  210  to the contact pads not shown) on the filter element  205 . 
     The active semiconductor circuit  210  may, for example, be one or a combination of amplifiers, mixers, analog-to-digital converters and digital processors. Typically for a receiver, the active semiconductor circuit  210  will comprise an amplifier such as, but not limited to, an InP or GaAs HEMT, HBT, pHEMT, nHEMT, III-V heterostructure or monolithic microwave integrated circuit (MMIC) amplifier. Such amplifiers are well known in the art. An InP or GaAs pHEMT or nHEMT amplifier is typically preferred. Commercially available examples are available from a number of sources such as, for example, Miteq Inc. (Hauppauge, N.Y. USA, Model No. SAFS1-01500200-08-CR-S) and Microwave Technology Inc. (Fremont, Calif. USA, Model No. SG0-7446, Part No. 01-50- 660).    
     The cryogenic source of the cryogenic device provides cooling to the cryogenic electronic components. The cryogenic source can, if the device is deployed in outer space, be the ambient outer space conditions, but the cryogenic source is typically a miniature cryocooler unit  230  of the appropriate size and power requirements. Such miniature cryocoolers are typically Stirling cycle machines such as those described in U.S. Pat. No. 4,397,155, EP-A-0028144, WO 90/12961 and WO 90/13710 (all of which are incorporated by reference as if fully set forth herein). 
     The above-described cryogenic devices can be utilized in a number of fields, and particularly in the wireless communications field in band-pass and band-reject filter applications. One such area is in a wireless communication base station receiver front-end in ground-based and tower top applications. General details on such uses can be found in the previously incorporated references. In such uses, the cryogenic front-end receiver of the present invention can be an integrated package similar in certain general respects to conventional units (such as depicted in FIG.  1 ), in that it comprises a cryogenic electronic unit and control circuitry in a single enclosure, which can be further electrically connected to other components of the base station either directly or remotely. Because of the inventive features of the cryogenic electronic unit described herein, however, the size, weight and power requirements of a front-end receiver in accordance with the present invention can be significantly reduced, in some cases by an order of magnitude or greater, while maintaining equivalent or even better performance, as compared to such conventional units. 
     The significant reduction in size, weight and power requirements makes the cryogenic devices in accordance with the present invention ideal for integration into, for example, antenna assemblies, satellite base stations, radar arrays and RF receivers. 
     A specific example of such includes an integrated antenna assembly, wherein the cryogenic device and at least one antenna of a wireless base station are assembled as an integrated unit. In contrast to systems depicted in previously incorporated U.S. Pat. No. 6,104,934, wherein the cryogenic electronic portion of the unit can be in close proximity to the antenna, the present inventions allows an integrated unit with the antenna even further reducing noise contamination to the system. 
     FIGS. 6A-6F represent several embodiments of a wireless communication base station and self-tuning cryogenic front-end receiver. FIG. 6A depicts a schematic diagram of a wireless base station cryogenic receiver configuration including diversity antenna  605  and main antenna  610 . Diversity antenna  605  provides additional gain of approximately 3 db over that of the signal received via main antenna  610 . Main antenna  610  receives and transmits simultaneously, whereas diversity antenna only receives signals. The corresponding signals are transmitted directly to cryogenic unit  630  in the case of the diversity antenna  605  and to diplexer  615  for the main antenna  610  before being forwarded to the cryogenic unit  630 . 
     Diplexer  615  is comprised of filters  620  and  625  for separating the signal into its transmission signal component and the received signal component. The received signal component is then transmitted to the cryogenic unit  630 . In the general case, the transmission signal is not processed through the cryogenic unit, because of heating capacity constraints, but otherwise can be processed by the cryogenic unit  630 . In this embodiment cryogenic unit  630  is comprised of HTS filters  635  and  645  with amplifiers  640  and  650  respectively. Generally, amplifiers are low-noise-amplification (LNA) amplifiers. The filtered and amplified received signal is then forwarded to amplifiers  655  and  660  respectively and in the case of the main antenna  610  electrical pathway, diplexed with the transmission component of the signal by diplexer  665  comprised of filters  670  and  675  and then is transmitted to the base station. 
     FIG. 6B depicts a second embodiment of the wireless base station and cryogenic receiver configuration of the present invention. FIG. 6B differs from the embodiment depicted in FIG. 6A in that cryogenic units  630  and  680  are dedicated to the main antenna  610  signal and the diversity antenna  605  signal, respectively. This configuration provides for added reliability and also includes bypass circuits  642  and  692 , respectively, to further insure that if one or both cryogenic units  630  and  680  fail that the base station will still receive and process the RF signals. 
     FIG. 6C depicts a third embodiment of the wireless base station and cryogenic receiver configuration of the present invention, wherein the receive antenna  615  signal is the only signal that is processed by cryogenic unit  630 . Also depicted is transmit antenna  620 . Additionally, bypass circuit  642 , further includes a filter  644 , thus providing additional reliability and filtering along this path, not provided in either of the embodiments depicted in FIGS. 6A and 6B. 
     FIG. 6D depicts a fourth embodiment of the wireless base station and cryogenic receiver configuration of the present invention. FIG. 6D does not include the diversity antenna of the embodiments depicted in FIGS. 6A-6B and has no active semiconductor circuit, i.e., low-noise amplifier, inside the cryogenic unit. This embodiment includes bypass  642  without filter  644  of the embodiment shown in FIG. 6C, but functions in all other respects as the previous embodiments. 
     FIG. 6E depicts a fifth embodiment of the wireless base station and cryogenic receiver configuration of the present invention. FIG. 6E differs from the fourth embodiment in that it includes diplexer  665  in the circuit before the signal is forward to the remaining sections of the base station but, like the fourth embodiment, has no active semiconductor circuit, i.e., low-noise amplifier, inside the cryogenic unit. 
     FIG. 6F depicts a sixth embodiment of the wireless base station and cryogenic receiver configuration of the present invention. FIG. 6F depicts a configuration wherein only the receive antenna  615  signal is processed by cryogenic unit  630 . The embodiment further includes bypass circuit  642  with bypass filter  644  and a diplexer  665  before transmitting the processed signal to the remaining sections of the base station. This embodiment differs from the third embodiment shown in FIG. 6C in that the present embodiment has no active semiconductor circuit, i.e., low-noise amplifier, inside the cryogenic unit. 
     The reader should note that the above embodiments are exemplary and are not intended to limit the scope of the present invention. The present invention can be applied in any environment wherein RF signals (and particularly microwave) are received and broadcast, such as but not limited to, radar arrays, satellite installations (home or commercial) and wireless and cellular base stations. In such uses, the cryogenic devices in accordance with the present invention can provide one, two, three or even significantly higher dB gains in an output signal-to-noise ratio, depending on the use and component configuration. 
     It will be apparent to those skilled in the art that various modifications and variations can be made in the present invention and in construction of this invention without departing from the scope or intent of the invention. Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the invention being indicated by the following claims.