The advantages and possible pitfalls of using a generalized method of measuring and, based on these measurements, predicting the transient or steady-state thermal response characteristics of an electronic equipment designed to operate in a space environment are reviewed. The method requires generation of a set of thermal influence coefficients by test measurement in vacuo. A implified thermal mockup isused in this test. Once this data set is measured, temperatures resulting from arbitrary steady-state or time varying power profiles can be economically calculated with the aid of a digital computer
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The theory shown here can provide thermal stability criteria based on physics and a goal steady stat...
Component qualification and acceptance temperatures are derived from worst case thermal analyses and...
Analog computer program for predicting orbiting spacecraft external surface temperature
International audienceThe 3 Omega Method is a form of the transient line method for thermal characte...
One of the main challenge of satellite manufacturers is its fully safety and complete operational fu...
A thermal control system was designed for the Space Station Freedom (SSF) sensor/electronics box (SS...
That nonlinear least squares can be used to determine effective thermal conductivity was demonstrate...
The following document describes an example mission, which originated from a real life concept of an...
The following document describes an example mission, which originated from a real life concept of an...
The following document describes an example mission, which originated from a real life concept of an...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
A description of the methods used to measure component temperatures and heat-rejection rates in a si...
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The theory shown here can provide thermal stability criteria based on physics and a goal steady stat...
Component qualification and acceptance temperatures are derived from worst case thermal analyses and...
Analog computer program for predicting orbiting spacecraft external surface temperature
International audienceThe 3 Omega Method is a form of the transient line method for thermal characte...
One of the main challenge of satellite manufacturers is its fully safety and complete operational fu...
A thermal control system was designed for the Space Station Freedom (SSF) sensor/electronics box (SS...
That nonlinear least squares can be used to determine effective thermal conductivity was demonstrate...
The following document describes an example mission, which originated from a real life concept of an...
The following document describes an example mission, which originated from a real life concept of an...
The following document describes an example mission, which originated from a real life concept of an...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
There are always differences between the computer predicted temperatures of a spacecraft thermal mod...
A description of the methods used to measure component temperatures and heat-rejection rates in a si...
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The thermal model of electronic device (sizes 0.36 x 0.24 x 0.16 m, mass 4 kg), functioning in the c...
The theory shown here can provide thermal stability criteria based on physics and a goal steady stat...