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Phase II Final Report - NASA's Institute for Advanced Concepts

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Chapter 3.0 Vehicle Design<br />

3.5 Fuel Storage and Production<br />

100<br />

Carbon 13.8 MPa (2000 psi)<br />

Carbon 34.5 MPa (5000 psi)<br />

Carbon 68.9 MPa (10,000 psi)<br />

Titanium 13.8 MPa (2000 psi)<br />

Titanium 34.5 MPa (5000 psi)<br />

Titanium 68.9 MPa (10,000 psi)<br />

10<br />

1<br />

0.1 0.2 0.5 1 1.5 2<br />

0.1<br />

Hydrogen Mass Stored (kg)<br />

Figure 3-148: Spherical Pressure Tank Mass Constructed of Carbon and Titanium at<br />

Various Storage Pressures<br />

Figure 3-148 shows how the mass of the tank will vary with different construction materials.<br />

The curves were generated <strong>for</strong> titanium and carbon over a range of hydrogen storage masses.<br />

The effect of storage pressure on the tank mass is due to the compressibility factor, Equation 3-<br />

37, that was used. The change in storage pressure also has a significant effect on the volume (or<br />

tank radius) as would be expected. This effect is shown in Figure 3-149. This figure represents<br />

the same hydrogen storage volumes given in Figure 3-148. This demonstrates that storing<br />

hydrogen gas at high pressures will minimize volume with a lesser effect on the overall tank<br />

mass.<br />

183

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