Last evening I tried to convey the concept that the critical-command modules needed to be of low-power design to insure their operability during the occasional rather lengthy eclipse cooling of the spacecraft. My message apparently did not sink in. John reports that his design of such a U band receiver would be dissipating some 3.5W due to its bullet-proof nature against 3rd-order IM products needed for protection on the U band.
If we go forward with such a module of that nature, it will need to have thermal control tapes on it to provide a mean emittance of about e=0.45. In a 3 hour eclipse we can expect to see spaceframe temperatures down to -100°C (173K) or lower. With such an environment John's module would be expected to see temperatures down to at least -44°C, which is a bit frosty for electronics that are expected to provide the critical services of commanding the spacecraft. Such operating temperatures are not felt to be advisable for that service.
If John's module were of the 1W category, temperatures of the receiver could be expected to be in the range of -15°C to -20°C which would be more operable for the service.
The above numbers are, of course, based on estimates which will be confirmed after we have the new spaceframe fully designed and analyzed. The "warmer" temperatures of the lower power modules are those that have been experienced and measured by telemetry from AO-10 and AO-13. These projections are thus based on 25 years of experience in these design concepts.
Dick Jansson --------------------------- mailto:[email protected] [email protected] ---------------------------
