Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
The o<strong>the</strong>r new variables in equation (4-21) are <strong>the</strong> partial derivatives <strong>of</strong> specific enthalpy with respect to<br />
pressure and temperature. The Golkar model was written <strong>for</strong> a pressurant tank using helium gas, <strong>for</strong><br />
which <strong>the</strong>se derivatives were constant over <strong>the</strong> range <strong>of</strong> pressures and temperatures experienced [42].<br />
However, <strong>the</strong>se partial derivatives were not constant <strong>for</strong> nitrogen over <strong>the</strong> range <strong>of</strong> conditions expected<br />
in <strong>the</strong> TALARIS CGSE tanks. This difference is illustrated in Figure 4-1.<br />
Figure 4-1. Enthalpy relations <strong>for</strong> helium and nitrogen.<br />
(a) Helium specific enthalpy vs. pressure [42]. (b) Nitrogen specific enthalpy vs. pressure.<br />
(c) Helium specific enthalpy vs. temperature [42]. (d) Nitrogen specific enthalpy vs. temperature.<br />
In Figure 4-1(a), <strong>the</strong> plots <strong>of</strong> specific enthalpy vs. pressure <strong>for</strong> helium are all linear with <strong>the</strong> same slope<br />
regardless <strong>of</strong> temperature, which shows that