Books on the topic 'Hypervelocity impact'

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1

J, Bean Alan, Darzi Kent, University of Alabama in Huntsville. Dept. of Mechanical Engineering., George C. Marshall Space Flight Center., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Hypervelocity impact physics. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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2

Hypervelocity gouging impacts. Reston, Va: American Institute of Aeronautics and Astronautics, 2009.

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3

Wilbeck, J. S. Experience with techniques for characterizing debris generated during hypervelocity impact testing. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

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4

K, Nahra Henry, and Lewis Research Center, eds. Hypervelocity impact testing of nickel hydrogen battery cells. [Cleveland, Ohio]: National Aeronautics and Space Administration, [Lewis Research Center, 1996.

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5

Piekutowski, A. J. Formation and description of debris clouds produced by hypervelocity impact. Huntsville, Ala: George C. Marshall Space Flight Center, 1996.

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6

Elfer, N. C. Structural damage prediction and analysis for hypervelocity impacts - handbook. Huntsville, Ala: George C. Marshall Space Flight Center, 1996.

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7

Stellingwerf, Robert Francis. Impact modeling with smooth particle hydrodynamics. Loa Alamos, NM: Los Alamos National Laboratory, 1993.

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8

Elfer, N. C. User's manual for space debris surfaces (SD_SURF). Huntsville, Alabama: George C. Marshall Space Flight Center, 1996.

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9

Manuelpillai, Gerald N. Space hypervelocity microparticle impact damage in polymer matrix composites. Ottawa: National Library of Canada, 1993.

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10

M, Curry Donald, and Lyndon B. Johnson Space Center., eds. Oxidation of reinforced carbon-carbon subjected to hypervelocity impact. Houston, Tex: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 2000.

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11

P, Fahrenthold Eric, and United States. National Aeronautics and Space Administration., eds. Design of orbital debris shields for oblique hypervelocity impact. [Washington, DC: National Aeronautics and Space Administration, 1994.

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12

George C. Marshall Space Flight Center., ed. Hypervelocity impact effects on solar cells: Final technical report. Huntsville, Al: NASA, Marshall Space Flight Center, 1993.

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13

R, Best Steve, Myre Craig A, and United States. National Aeronautics and Space Administration., eds. Hypervelocity impact testing of Space Station Freedom solar cells. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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14

Schonberg, William P. Predicting multi-wall structural response to hypervelocity impact using the HULL code. Huntsville, Ala: George C. Marshall Space Flight Center, 1993.

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15

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Predicting multi-wall structural response to hypervelocity impact using the Hull Code. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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16

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Predicting multi-wall structural response to hypervelocity impact using the Hull Code. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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17

Lamontagne, Chantal G. Hypervelocity impact damage to polymer matrix composite structures in space. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

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18

B, Hayashida K., and George C. Marshall Space Flight Center., eds. Empirical predictions of hypervelocity impact damage to the space station. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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19

B, Hayashida K., and George C. Marshall Space Flight Center., eds. Empirical predictions of hypervelocity impact damage to the space station. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1991.

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20

A, Taylor Roy, Horn Jennifer R, and George C. Marshall Space Flight Center., eds. An analysis of penetration and ricochet phenomena in oblique hypervelocity impact. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1988.

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21

E, Anderson Charles, United States. Defense Advanced Research Projects Agency., and Hypervelocity Impact Symposium (1986 : San Antonio, Tex.), eds. Hypervelocity impact: Proceedings of the 1986 symposium, San Antonio, Texas, 21-24 October 1986. Oxford: Pergamon Press, 1987.

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22

Griffis, D. P. Analysis of Interplanetary Dust Experiment detectors and other witness plates^Elemental analyses of hypervelocity microparticle impact sites on Interplanetary Dust Experiment sensor surfaces^Contaminant interferences with SIMS analyses of microparticle impactor residues on LDEF surfaces. Raleigh, N. C: North Carolina State University, 1992.

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23

Serrano, J. Vulnerability of Space Station Freedom modules: A study of the effects of module perforation on crew and equipment. Huntsville, Ala: Marshall Space Flight Center, 1996.

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24

United States. National Aeronautics and Space Administration., ed. Final report submitted to National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ... for research entitled Coupling of SPH and finite element codes for multi-layer orbital debris shield design. Austin, TX: Dept. of Mechanical Engineering, University of Texas, 1997.

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25

Visentine, James T. In-space technology development: atomic oxygen and orbital debris effects. Houston, Tex: Lyndon B. Johnson Space Center, 1989.

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26

United States. National Aeronautics and Space Administration., ed. Orbital impacts and the space shuttle windshield. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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27

Company, Barringer Crater, Lunar and Planetary Institute, and United States. National Aeronautics and Space Administration., eds. Papers presented to the International Conference on Large Meteorite Impacts and Planetary Evolution: August 31-September 2, 1992, Sudbury, Ontario, Canada. Houston, Tex: The Institute, 1992.

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28

Company, Barringer Crater, Lunar and Planetary Institute, and United States. National Aeronautics and Space Administration., eds. Papers presented to the International Conference on Large Meteorite Impacts and Planetary Evolution: August 31-September 2, 1992, Sudbury, Ontario, Canada. Houston, Tex: The Institute, 1992.

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29

H, Robinson J., Hill S. A, and George C. Marshall Space Flight Center., eds. SEDS tether M/OD damage analyses. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1997.

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30

United States. National Aeronautics and Space Administration., ed. Oblique hypervelocity impact simulation for multi-layer orbital debris shielding (NAG 9-744): Final report. [Washington, DC: National Aeronautics and Space Administration, 1996.

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31

United States. National Aeronautics and Space Administration., ed. Oblique hypervelocity impact simulation for multi-layer orbital debris shielding (NAG 9-744): Final report. [Washington, DC: National Aeronautics and Space Administration, 1996.

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32

Takata, Toshiko. Impact of Comet Shoemaker-Levy-9 on Jupiter. [Washington, DC: National Aeronautics and Space Administration, 1994.

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33

Takata, Toshiko. Impact of Comet Shoemaker-Levy-9 on Jupiter. [Washington, DC: National Aeronautics and Space Administration, 1994.

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34

Chamis, C. C. Computational engine structural analysis. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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35

Mog, R. A. Global nonlinear optimization of spacecraft protective structures design. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1990.

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36

United States. National Aeronautics and Space Administration., ed. Optimization techniques applied to passive measures for in-orbit spacecraft survivability. Huntsville, AL: SAIC, 1991.

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37

Marvin, Price D., and United States. National Aeronautics and Space Administration., eds. Optimization techniques applied to passive measures for in-orbit spacecraft survivability. [Washington, DC?: National Aeronautics and Space Administration, 1988.

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38

J, Helba Michael, Hill Janeil B, and United States. National Aeronautics and Space Administration., eds. Optimization techniques applied to passive measures for in-orbit spacecraft survivability: Final report. Huntsville. Ala: Science Applications International Corporation, 1992.

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39

V, Giridharan, and United States. National Aeronautics and Space Administration., eds. MLITEMP: A computer program to predict the thermal effects associated with hypervelocity impact damage to the Space Station MLI. [Washington, DC: National Aeronautics and Space Administration, 1991.

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40

F, Grieve Richard A., and United States. National Aeronautics and Space Administration., eds. Scaling impact-melt and crater dimensions: Implications for the lunar cratering record. [Washington, DC: National Aeronautics and Space Administration, 1997.

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41

F, Grieve Richard A., and United States. National Aeronautics and Space Administration., eds. Scaling impact-melt and crater dimensions: Implications for the lunar cratering record. [Washington, DC: National Aeronautics and Space Administration, 1997.

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42

F, Grieve Richard A., and United States. National Aeronautics and Space Administration., eds. Scaling impact-melt and crater dimensions: Implications for the lunar cratering record. [Washington, DC: National Aeronautics and Space Administration, 1997.

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43

F, Grieve Richard A., and United States. National Aeronautics and Space Administration., eds. Scaling impact-melt and crater dimensions: Implications for the lunar cratering record. [Washington, DC: National Aeronautics and Space Administration, 1997.

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44

United States. National Aeronautics and Space Administration., ed. Biospheric effects of a large extraterrestrial impact: Case study of the Cretaceous/Tertiary boundary crater : FY 1993 progress report. La Canada, CA: Geo Eco Arc Research, 1994.

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45

United States. National Aeronautics and Space Administration., ed. Biospheric effects of a large extraterrestrial impact: Case study of the Cretaceous/Tertiary boundary crater : FY 1993 progress report. La Canada, CA: Geo Eco Arc Research, 1994.

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46

United States. National Aeronautics and Space Administration., ed. Asteroid entry in Venusian atmosphere: Pressure and density fields effect on crater formation : final report. [Seattle, Wash.]: Boeing Defense & Space Group, 1995.

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47

International Symposium on Explosion, Shock Wave and Hypervelocity Phenomena (2nd 2007 Kumamoto, Japan). Explosion, shock wave and hypervelocity phenomena in materials II: Selected peer reviewed papers from the 2nd International Symposium on Explosion, Shock Wave and Hypervelocity Phenomena (ESHP-2), 6-9 March 2007, Kumamoto, Japan. Stafa-Zurich, Switzerland: Trans Tech Publications, 2008.

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48

B, Hayeshida K., and George C. Marshall Space Flight Center., eds. SUNSPOT: A program to model the behavior of hypervelocity impact damaged multilayer insulation in the Sunspot thermal vacuum chamber of Marshall Space Flight Center. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1992.

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49

Center, Langley Research, ed. Development of metallic thermal protection systems for the reusable launch vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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50

United States. National Aeronautics and Space Administration., ed. Final report submitted to National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, Space Science Branch ... for research entitled Hypervelocity impact simulation for micrometeorite and debris shield design. [Washington, DC: National Aeronautics and Space Administration, 1992.

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