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035     |z(NjP)Voyager6794274
040    GPO |beng |cGPO |dMvI
049    DOCS
074    0830-H-15 (online)
086 0  NAS 1.60:2011-216457
090    Electronic Resource
100 1  Nettles, A. T. |q(Alan T.)
245 14 The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles / |cA.T. Nettles, A.J. Hodge, and J.R. Jackson.
264  1 [Huntsville], Ala. : |bNational Aeronautics and Space Administration, Marshall Space Flight Center, |c[2011]
300    1 online resource (vii, 23 pages) : |billustrations.
336    text |btxt |2rdacontent
337    computer |bc |2rdamedia
338    online resource |bcr |2rdacarrier
490 1  NASA/TP ; |v2011-216457
500    Title from title screen (viewed on Aug. 2, 2011).
500    "February 2011."
504    Includes bibliographical references (pages 22-23).
650  7 Damage assessment. |2nasat
650  7 Launch vehicles. |2nasat
650  7 Thermal protection. |2nasat
650  7 Sandwich structures. |2nasat
650  7 Residual strength. |2nasat
650  7 Ares 1 launch vehicle. |2nasat
650  7 Composite structures. |2nasat
650  7 Composite materials. |2nasat
650  7 Impact damage. |2nasat
700 1  Hodge, A. J.
700 1  Jackson, J. R.
710 2  George C. Marshall Space Flight Center.
830  0 NASA technical paper ; |v216457.
945    DOCS |cNAS 1.60:2011-216457
956 40  |uhttps://purl.fdlp.gov/GPO/gpo10728