Preliminary feasibility studies based on breakeven refrigeration thermodynamics, have been conducted for candidate power conditioning components in a transportable radar power system (Donovan, B.D. et al., 1995 “Effects of Refrigeration in a Transportable Cryogenic Aerospace Application,” Proc. 30th IECEC, Vol. 1, pp. 473–478; Ramalingam, M. et al., 1996 “Systems Analysis for a Cryogenic Aerospace Terrestrial Radar Power System,” Proc. 31st IECEC, Vol. 1). The analysis based on breakeven refrigeration thermodynamics revealed that in the case of a general switching device such as a power MOSFET, it would be more beneficial to operate it at 150 to 220 K, using a Stirling cycle-based cryocooler. The overall system efficiency was jeopardized by way of large input power requirements to cool small heat loads at lower temperatures, while the performance of the device itself suffered at higher temperatures. The break-even refrigeration thermodynamic analysis was also applied to multilayer ceramic capacitors at cryogenic temperatures. It was found that in order to avoid a power penalty for cooling the capacitor to 77 K, the cryocooled equivalent series resistance (ESR) value would have to be a factor of 40 lower than that of a conventional capacitor ESR value if using a Gifford-McMahon (GM) cooling cycle. A factor of 12 better improvement in ESR is required for a yet-to-be-developed more efficient Stirling cycle. In this paper, this break-even thermodynamic analytical concept was then partially extended from the component level to the radar power system level. The entire power system was sized based on several combinations of cryocooled generators, power conditioning, and antenna equipment. The analysis revealed that even though the radar output could potentially be increased two-to threefold by the introduction of cryocooled technologies, the sizes of the coolers begin to negate these advantages. Several power systems were evaluated with reference to a common figure-of-merit to arrive at an optimum configuration. [S0195-0738(00)00803-7]

1.
Fingers, R. T., and Oberly, C. E., 1991, “Implications of High Temperature Superconductors for Power Generation,” 26th IECEC, Vol. 4, Boston, MA, pp. 564–569.
2.
Oberly
,
C. E.
,
1977
, “
Air Force Applications of Lightweight Superconducting Machinery
,”
IEEE Trans. Magn.
,
MAG-13
, pp.
260
268
.
3.
Ramalingam, M. L., Donovan, B. D., Lamp, T. R., and Beam, J. E., 1996, “Systems Analysis For A Cryogenic Aerospace Terrestrial Radar Power System,” Proc., 31st IECEC, Vol. 1.
4.
Donovan, B. D., Mahefkey, E. T., and Ramalingam, M. L., 1995, “Effects of Refrigeration in a Transportable Cryogenic Aerospace Application,” Proc., 30th IECEC, Vol. 1, pp. 473–478.
5.
Foty
,
D. P.
,
1990
, “
Impurity Ionization in MOSFETs at Very Low Temperatures
,”
Cryogenics
,
30
, pp.
1056
1063
.
6.
Mueller
,
O.
,
1990
, “
Switching Losses of the Cryogenic MOSFET and SIT
,”
Cryogenics
,
30
, pp.
1094
1100
.
7.
Sze, S. M., 1985, Semiconductor Devices: Physics and Technology, Wiley, New York.
8.
Pires
,
R. G.
,
Dickstein
,
R. M.
,
Titcomb
,
S. L.
, and
Anderson
,
R. L.
,
1990
, “
Carrier Freeze Out in Silicon
,”
Cryogenics
,
30
, pp.
1064
1068
.
9.
Kirschmour, R. K., 1986, Low Temperature Electronics, IEEE Press, New York.
10.
Mueller
,
O.
,
1989
, “
On-Resistance, Thermal Resistance and Reverse Recovery Time of Power MOSFETs at 77K
,”
Cryogenics
,
29
, pp.
1006
1014
.
11.
Mueller, O., 1991, “Cryogenic Power Conversion—Combining HT Superconductors and Semiconductors,” AIP Conference Proc. 251, Am. Inst. Phys., New York, NY.
12.
Lawless, W. N., 1992, “Cryogenic Ceramic Multilayer Capacitors,” USAF Technical Report, CeramPhysics, Inc., WL-TR-92-2124.
13.
Mathes, K. N., and Minnich, S. H., 1965, “Cryogenic Capacitor Investigation,” General Electric Co., Final Report, S-67-1095.
14.
Schempp, E., and Jackson, W. D., 1996, “System Considerations in Capacitive Energy Storage,” Proc., 31st IECEC, Vol. 2, pp. 666–671.
15.
Moynihan, J. D., 1987, “Selection and Application of Capacitors,” Components Technology Institute, Inc.
16.
Donovan, B. D., Ramalingam, M. L., and Mahefkey, E. T., 1995, “Refrigeration Penalties for Cryocooling Power Semiconductor Devices,” ASME National Heat Transfer Conference, Portland, OR.
17.
Harris, M., Lasker, J., Gebara, E., and Kikel, T., 1998, “Development of Cryogenic Measurement Techniques for Microwave Power Amplifiers,” 33rd IECEC, Colorado Springs, CO.
18.
Ackermann
,
R. A.
,
1993
, “
Closed Cycle Refrigeration for SC Application
,”
Superconductor Industry
,
3
, pp.
15
24
.
19.
Barron, R., 1966, Cryogenic Systems, McGraw Hill, New York.
20.
Walker, G., 1983, Cryocoolers. Part 1: Fundamentals, Plenum Press, New York.
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