Books on the topic '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.
Find full textCobleigh, Brent R. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: Dryden Flight Research Center, 1998.
Find full textNASA 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.
Find full textNASA 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.
Find full textGeorge 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.
Find full textUnited 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.
Find full textCenter, 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.
Find full textWood, William A. Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textAmerican Institute of Aeronautics and Astronautics. Recommended practice: Space launch integration. Reston, VA: American Institute of Aeronautics and Astronautics, 2001.
Find full textJ, 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.
Find full textKarp, K. A. Sintez vseazimutalʹnykh raket-nositeleĭ. Moskva: Moskovskiĭ gos. aviat︠s︡ionnyĭ institut (tekhnicheskii universitet), 2007.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: Lyndon B. Johnson Space Center, 1997.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Find full textJames P. Smith - undifferentiated. X- 38 vehicle 131 flutter assessment. Washington, D.C: National Aeronautics and Space Administration, 1997.
Find full textJames P. Smith - undifferentiated. X-38 vehicle 131 flutter assessment. [Houston, Tex.]: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1997.
Find full textS, 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.
Find full textCenter, 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.
Find full textScott, 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.
Find full textCenter, 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.
Find full textShui 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.
Find full textL, 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.
Find full textKochetova, 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.
Full textOffice, 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.
Find full textDynamic response of a hammerhead launch vehicle wind-tunnel model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Find full textModel Predictive Control for Ascent Load Management of a Reusable Launch Vehicle. Storming Media, 2002.
Find full textDevelopment of the X-33 aerodynamic uncertainty model. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Find full textNational 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.
Find full textAeroheating predictions for X-34 using an inviscid-boundary layer method. Reston, VA: American Institute of Aeronautics and Astronautics, 1998.
Find full textAeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textAeroheating predictions for X-34 using an inviscid-boundary layer method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textAir 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.
Find full textAir 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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