NASA TN D-3784
The design range of output variables for the speed controller components is given in table I. As an example, at 400 cps the SCRa#39; s of all three control circuits are at a firing angle of 0Ad. Figure 7 shows that, at a firing angle of 0Ad, no power is anbsp;...
| Title | : | NASA TN D-3784 |
| Author | : | Roy C. Tew, Robert D. Gerchman, Herbert G. Hurrell, United States. National Aeronautics and Space Administration |
| Publisher | : | - 1967 |
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