Depressurization test method using pressure vessel
View Patent ↗Techniques for testing a component for compatibility with a depressurization profile associated with a launch vehicle payload fairing during ascent are disclosed. A pressure of air or other gas within a pressure vessel containing the component is raised to a first value substantially higher than one atmosphere absolute pressure. The air/gas pressure within the pressure vessel is lowered, by venting into the ambient atmosphere, at a rate simulating or demonstrating margin with respect to the launch vehicle payload fairing depressurization profile. The component is inspected for damage. The component may be a panel including a honeycomb core sandwiched between two faceskins, the panel having a planar area in excess of twenty five square feet.
1. A method comprising:
testing a component for compatibility with a depressurization profile associated with a launch vehicle ascent, the testing including:
raising a pressure within a pressure vessel containing the component to a first value not less than approximately two atmospheres absolute pressure;
lowering the pressure within the pressure vessel at a rate simulating the depressurization profile; and
inspecting the component for damage.
2. The method of claim 1 , wherein the component is a panel comprising a honeycomb core sandwiched between two faceskins.
3. The method of claim 2 , wherein a planar area of the panel is at least 25 square feet.
4. The method of claim 2 , wherein a planar area of the panel is at least 100 square feet.
5. The method of claim 1 , wherein the rate simulating the depressurization profile averages approximately 0.5 atmospheres per minute.
6. The method of claim 5 , wherein lowering the pressure within the pressure vessel at the rate of approximately 0.5 atmospheres per minute is performed for a duration of greater than one minute.
7. The method of claim 5 wherein lowering the pressure within the pressure vessel at the rate of approximately 0.5 atmospheres per minute is performed by venting the pressure vessel to a pressure no less than ambient pressure.
8. The method of claim 1 , wherein the rate simulating the depressurization profile has a maximal value of at least one atmosphere per minute.
9. The method of claim 1 , wherein raising the pressure results in achieving substantially equal pressures in the pressure vessel exterior to the component and in interior portions of the component.
10. The method of claim 1 , wherein the pressure vessel is an autoclave.
11. A method comprising:
testing a component for compatibility with a depressurization profile associated with a launch vehicle ascent, the depressurization profile including a maximum expected ascent depressurization rate, the testing including:
raising a pressure within a pressure vessel containing the component to a first value not less than approximately two atmospheres absolute pressure;
lowering the pressure within the pressure vessel at a test depressurization rate that is greater than the maximum expected ascent depressurization rate; and
inspecting the component for damage.
12. The method of claim 11 , wherein the test depressurization rate is 1.5 times higher than the maximum expected ascent depressurization rate.
13. The method of claim 11 , wherein the component is a panel comprising a honeycomb core sandwiched between two faceskins.
14. The method of claim 11 , wherein the test depressurization rate averages at least 0.5 atmospheres per minute.
15. The method of claim 11 , wherein lowering the pressure within the pressure vessel at the test depressurization rate is performed for a duration of greater than one minute.
16. The method of claim 11 , wherein the test depressurization rate has a maximal value of at least one atmosphere per minute.
17. The method of claim 16 , wherein lowering the pressure within the pressure vessel includes venting the pressure vessel to a pressure no less than ambient pressure.
18. The method of claim 11 , wherein raising the pressure results in achieving substantially equal pressures in the pressure vessel exterior to the component and in interior portions of the component.
19. The method of claim 11 , wherein the pressure vessel is an autoclave.