For example, avionic systems must sustain acceptable performance over relatively large variations in body force created by ... On the other hand, space vehicle cooling hardware designed at one-G conditions must endure the microgravity .... of 1300 W/cm2 (Mudawar et al., 1985). ... The thermocouple and heater lead wires were sows*Ad amBBBBM Pressure Tap Fig.l Schematic diagram of the rotating 68.
|Title||:||Heat transfer in electronics, 1989|
|Author||:||R. K. Shah, American Society of Mechanical Engineers. Heat Transfer Division|
|Publisher||:||Amer Society of Mechanical - 1989|