Libros sobre el tema "Launch Vehicle Model"
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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.
Buscar texto completoCobleigh, Brent R. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: Dryden Flight Research Center, 1998.
Buscar texto completoNASA 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.
Buscar texto completoNASA 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.
Buscar texto completoGeorge 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.
Buscar texto completoUnited 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.
Buscar texto completoCenter, 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.
Buscar texto completoWood, William A. Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoAmerican Institute of Aeronautics and Astronautics. Recommended practice: Space launch integration. Reston, VA: American Institute of Aeronautics and Astronautics, 2001.
Buscar texto completoJ, Vess Robert, North Carolina State University. Dept. of Mechanical and Aerospace Engineering. y 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.
Buscar texto completoKarp, K. A. Sintez vseazimutalʹnykh raket-nositeleĭ. Moskva: Moskovskiĭ gos. aviat︠s︡ionnyĭ institut (tekhnicheskii universitet), 2007.
Buscar texto completoJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: Lyndon B. Johnson Space Center, 1997.
Buscar texto completoJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Buscar texto completoJames P. Smith - undifferentiated. X- 38 vehicle 131 flutter assessment. Washington, D.C: National Aeronautics and Space Administration, 1997.
Buscar texto completoJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Buscar texto completoS, Guarro, Apostolakis G y 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.
Buscar texto completoCenter, 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.
Buscar texto completoScott, McRae D., Bond Ryan B y 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.
Buscar texto completoCenter, 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.
Buscar texto completoShui 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.
Buscar texto completoL, Kleb William, Alter Steven J y 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.
Buscar texto completoKochetova, Zhanna, Natal'ya Maslova y Oleg Bazarskiy. Aviation and missile clusters and the environment. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1544137.
Texto completoOffice, 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.
Buscar texto completoDynamic response of a hammerhead launch vehicle wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Buscar texto completoModel Predictive Control for Ascent Load Management of a Reusable Launch Vehicle. Storming Media, 2002.
Buscar texto completoDevelopment of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Buscar texto completoNational Aeronautics and Space Administration y NASA. Lateral Vibration Characteristics of a 1/40-Scale Dynamic Model of Apollo-Saturn V Launch Vehicle: November 1 1968. Independently Published, 2022.
Buscar texto completoAeroheating predictions for X-34 using an inviscid-boundary layer method. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.
Buscar texto completoAeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoAeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completoAir 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.
Buscar texto completoAir 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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