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NASA Technical Reports Server (NTRS) 20060026037: Guidelines for the Utilization of Composite Materials in Oxygen Storage Tanks PDF

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Preview NASA Technical Reports Server (NTRS) 20060026037: Guidelines for the Utilization of Composite Materials in Oxygen Storage Tanks

Source of Acquisition NASA Marshall Space night center Guidelinesf or the Utilization of Composite Materials in Oxygen Storage Tanks Space travel is inherently dangerous and, currently, quite expensive. NASA has always done everything possible to minimize the risk associated with the materials chosen for space travel applications by requiring that all materials associated with NASA programs meet the strict requirements established by NASA testing standard NASA-STD-6001 Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Materials in Environments that Support Combustion. NASA also has the need to develop lighter weight structural materials that will allow more payload weight to be carried into space. NASA is utilizing composite materials inside the orbiter to lighten the overall weight, but has not considered composite materials for oxygen tanks because of the inherent incompatibility of composite materials with atomic oxygen. This presentation will focus on how oxygen tanks can be built from composite materials. Details will be provided for the design and compatibility testing techniques that will be utilized to create a new NASA standard, NASA-HDBK-60 18 , which will serve as the starting point for the design of oxygen tanks made from composite materials. zlr S 0 ai rn L s a, F .c.r z S .c.r 8 cd a, L ti L. 0 .6-: E a, 51 a, s 0 0 L .c.r 0 .S-T : L S cd a, W ti 0 .c.r cn S c S 12 a, LLI 8 0 s cd 0 z- a L .I_ I .0- cn Q c 9.c.r a, cf) a, cn cn cf) LL a, a, # 0 0 0 k cb 111 cn a, 0 0 cd am - c G 1cz cn z W .c-d L z a, CI 9 P a v) cf) a 0 a, E . cn S a a . J2 0 0 E a, c> cn S a, 0 U cn Q .0 cn a, .k a, C U 0 m m- >r 0 1 . cn c> L Q I- 0 C . 0 3 a . C C € L 0 0 S L - a, I. I. I cn a, E cn a c) . 23 S I- L c) a, a, 0 L a U 0 € I cn . . c) cd S cnn 0 . 0 3 a, 0 S L m- cd a, a, E Ts) L S cd S cd a, m- > cn U cd cn cd cn I 2 S E a, Ts) S Ts) .a, I > 0 3 X S . 0 c cd a, CCI . m- 0 c S 3 cd .Ts) - cn cd . Q L cd 0 13 . ,/ cn I- cn c) a, I- 5 a, C Q cn u, m- u, 3 a, 0 a, c) c S L. 0 0 L a, CI c a, a c) c U- 13 a 0 - 0 h a Q .- - U S 3 a I 0 Q L (I) Q 0 0 0 0- 7 e3 3 S a, * Ts) X 0 L a, .L C I- a, .1 c 0 . 0 8 S a, cn I. c u) I-X 0 a . . a, e= IC1 a, cn U I-L L .a, a, * L a, Q a 13 I- U . C. a, c) a, E cn S a, U a, c S I- m .0 a C . a a, .1 . C. a, I- a, cnh 0 c cn c S cn E cn Ts) a, c . L I-c n 2 a, a, a, 3 E S U c) a Ts) x 3 0 cn c U c) S a, a 0 U U I . a, m- cn a I-c n . a, 0 a E cn a m- . 3 0 .m a, a, c) + 12 S . a L 0 m- a 3 cn 12 Q S E U a, S 0 a ez c) 0 cn E S 0 =E L m m Z 0 I- c) a, .% L. L a, a r a -cn E a .ch m- L m- a, Q L a, a, a % c X € t- 0 e- 2 a, c a, 1a > 0 c x - 0 a, a, 1 L L a a a, 0 m 3 m- cn - Ia S a a cn Q 1 a, E I- L a, a, c m- cn 0 - Ia c) 1 1 0 E Q h 1a S a l a , t .-- c D 0 I I- il) cn % c) X Q a, 0 E > E E 0 0 -a, c 0 L +- 8- 1 c) a, 0 8- is m 0 a, E U c a, a a, a, 0 a, € cn S 0 a, U 0 c > n c I a a c c a, c 0 a, cn . 1 0 L 0 cn - a, 10 Is- C a cn 4 z S 0 Q 3 T3 a, u) cd m a, + 2 a, + 2 1 7 A A A U 0 c s +

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