Books on the topic 'Launch Vehicle Model'

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1

NASA Dryden Flight Research Center., ed. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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2

Cobleigh, Brent R. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: Dryden Flight Research Center, 1998.

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3

NASA Dryden Flight Research Center., ed. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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4

NASA Dryden Flight Research Center., ed. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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5

George C. Marshall Space Flight Center., ed. A strategy for integrating a large finite element model using MSC NASTRAN/PATRAN: X-33 lessons learned. [Huntsville, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

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6

United States. National Aeronautics and Space Administration., ed. A transient model of the RL10A-3-3A rocket engine. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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7

Center, Langley Research, ed. Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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8

Wood, William A. Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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9

American Institute of Aeronautics and Astronautics. Recommended practice: Space launch integration. Reston, VA: American Institute of Aeronautics and Astronautics, 2001.

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10

J, Vess Robert, North Carolina State University. Dept. of Mechanical and Aerospace Engineering., and Langley Research Center, eds. Design and fabrication of the NASA HL-20 full scale research model. Raleigh, NC: North Carolina State University, Mechnical and Aerospace Engineering, Mars Mission Research Center, 1991.

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11

Karp, K. A. Sintez vseazimutalʹnykh raket-nositeleĭ. Moskva: Moskovskiĭ gos. aviat︠s︡ionnyĭ institut (tekhnicheskii universitet), 2007.

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12

James P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: Lyndon B. Johnson Space Center, 1997.

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13

James P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.

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14

James P. Smith - undifferentiated. X- 38 vehicle 131 flutter assessment. Washington, D.C: National Aeronautics and Space Administration, 1997.

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15

James P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.

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16

S, Guarro, Apostolakis G, and United States. National Aeronautics and Space Administration., eds. Demonstration of the dynamic flowgraph methodology using the Titan II space launch vehicle digital flight control system. Los Angeles, CA: Mechanical, Aerospace, and Nuclear Engineering Dept., University of California, 1994.

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17

Center, Langley Research, ed. Surface modeling and grid generation of orbital sciences X34 vehicle (phase I): Under contract NAS1-96014. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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18

Scott, McRae D., Bond Ryan B, and NASA Glenn Research Center, eds. Three dimensional numerical simulation of rocket-based combined-cycle engine response during mode transition events. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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19

Center, Lewis Research, ed. Modification of the SHABERTH bearing code to incorporate RP-1 and a discussion of the traction model. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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20

Shui xia yun zai qi xing neng de fen xi yu she ji: Analysis and design of performance of underwater launched capsules. Beijing Shi: Guo fang gong ye chu ban she, 2008.

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21

L, Kleb William, Alter Steven J, and United States. National Aeronautics and Space Administration., eds. Aeroheating predictions for X-34 using an inviscid-boundary layer method. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.

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22

Kochetova, Zhanna, Natal'ya Maslova, and Oleg Bazarskiy. Aviation and missile clusters and the environment. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1544137.

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Abstract:
The monograph introduces a new concept - the aviation and missile cluster as a new class of objects of geo-ecological monitoring, united by the solution of identical strategic tasks of the state, the interconnection of its structural elements, the identity of priority contaminants and products of their transformation. The scientific and methodological apparatus of complex geoecological monitoring of territories under the influence of objects of aviation and space activities is presented, including predictive models of the spread and transformation of priority contaminants in environmental objects, taking into account their physical and chemical properties, geographical and climatic features of the studied territory; algorithms and methods for assessing the environmental situation in the area of the aviation and rocket cluster to support management decisions on conducting rehabilitation and preventive medical and environmental measures. The proposed scientific and methodological apparatus improves the quality of the assessment of the geoecological situation while reducing the cost of monitoring the territory of the aviation and missile cluster. The scientific results obtained by the authors based on the results of eleven-year geoecological monitoring of a typical aviation and rocket cluster located within the city of Voronezh and including an airfield of state aviation and a test complex of launch vehicles are presented. For a wide range of readers interested in environmental problems of scientific and technological progress.
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23

Office, General Accounting. Air pollution: Prior indoor air quality problems at the National Institute of Environmental Health Sciences : report to the Honorable Lauch Faircloth, U.S. Senate. Washington, D.C. (P.O. Box 37050, Washington, D.C. 20013): The Office, 1998.

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24

Dynamic response of a hammerhead launch vehicle wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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25

Model Predictive Control for Ascent Load Management of a Reusable Launch Vehicle. Storming Media, 2002.

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26

Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.

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27

National Aeronautics and Space Administration and NASA. Lateral Vibration Characteristics of a 1/40-Scale Dynamic Model of Apollo-Saturn V Launch Vehicle: November 1 1968. Independently Published, 2022.

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28

Aeroheating predictions for X-34 using an inviscid-boundary layer method. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.

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29

Aeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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30

Aeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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31

Air pollution: Prior indoor air quality problems at the National Institute of Environmental Health Sciences : report to the Honorable Lauch Faircloth, U.S. Senate. Washington, D.C. (P.O. Box 37050, Washington, D.C. 20013): The Office, 1998.

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32

Air pollution: Prior indoor air quality problems at the National Institute of Environmental Health Sciences : report to the Honorable Lauch Faircloth, U.S. Senate. Washington, D.C. (P.O. Box 37050, Washington, D.C. 20013): The Office, 1998.

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