Livres sur le sujet « Single stage design »
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American Institute of Aeronautics and Astronautics., Langley Research Center et International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, Tenn.), dir. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C : American Institute of Aeronautics and Astronautics, 1995.
Trouver le texte intégralAmerican Institute of Aeronautics and Astronautics. et International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, TN).), dir. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C : American Institute of Aeronautics and Astronautics, 1995.
Trouver le texte intégralCenter, NASA Glenn Research, dir. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
Trouver le texte intégralCenter, NASA Glenn Research, dir. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
Trouver le texte intégralCenter, NASA Glenn Research, dir. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
Trouver le texte intégralMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 2001.
Trouver le texte intégralMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 2001.
Trouver le texte intégralMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 2001.
Trouver le texte intégralMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 2001.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Requirements report for SSTO vertical take-off/horizontal landing vehicle. [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralOvtov, Vladimir. Machine parts. Course design. ru : INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1171976.
Texte intégralUnited States. National Aeronautics and Space Administration., dir. 1994 NASA/USRA/ADP design projects : Final report. [Washington, DC : National Aeronautics and Space Administration, 1994.
Trouver le texte intégralCruse, Thomas. 1994 NASA/USRA/ADP design projects : Final report, NASw-4435. [Washington, DC : National Aeronautics and Space Administration, 1994.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Selection process for trade study : Reusable hydrogen composite tank system (RHCTS). [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Trade study plan for reusable hydrogen composite tank system (RHCTS). [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Test plans, GCPS task 4, subtask 4.2, thrust structure development. [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems : Final report. [Washington, D.C : National Aeronautics and Space Administration, 1995.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Advances in hypersonic vehicle synthesis with application to studies of advanced thermal protection systems : Final report. [Washington, D.C : National Aeronautics and Space Administration, 1995.
Trouver le texte intégralH, Levack Daniel J., Nixon Robert F et United States. National Aeronautics and Space Administration., dir. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C : American Institute of Aeronautics and Astronautics, 1994.
Trouver le texte intégralH, Levack Daniel J., Nixon Robert F et United States. National Aeronautics and Space Administration., dir. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C : American Institute of Aeronautics and Astronautics, 1994.
Trouver le texte intégralH, Levack Daniel J., Nixon Robert F et United States. National Aeronautics and Space Administration., dir. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C : American Institute of Aeronautics and Astronautics, 1994.
Trouver le texte intégralGallaher, M. A guidance and control assessment of three vertical landing options for RLV. MSFC, Ala : National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.
Trouver le texte intégralErich, Espenschied, Klop Jeffrey et United States. National Aeronautics and Space Administration., dir. The control system for the X-33 linear aerospike engine. [Washington, DC : National Aeronautics and Space Administration, 1998.
Trouver le texte intégralErich, Espenschied, Klop Jeffrey et United States. National Aeronautics and Space Administration., dir. The control system for the X-33 linear aerospike engine. [Washington, DC : National Aeronautics and Space Administration, 1998.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Milestone 4 : Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralUnited States. National Aeronautics and Space Administration., dir. Milestone 4 : Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralNew York (State). Dept. of Audit and Control. Division of Management Audit. Office of Mental Retardation and Developmental Disabilities : A cost comparison : community-based residences vs. single-family homes. [Albany?] : The Division, 1993.
Trouver le texte intégralMoseley, V. J. "Jon", Andreas Lampropoulos, Eftychia Apostolidi et Christos Giarlelis. Characteristic Seismic Failures of Buildings. Sous la direction de Stephanos E. Dritsos. Zurich, Switzerland : International Association for Bridge and Structural Engineering (IABSE), 2019. http://dx.doi.org/10.2749/sed016.
Texte intégralUrunov, Asror. Regional economy. ru : INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1013012.
Texte intégralde Sá Caetano, Elsa. Cable Vibrations in Cable-Stayed Bridges. Zurich, Switzerland : International Association for Bridge and Structural Engineering (IABSE), 2007. http://dx.doi.org/10.2749/sed009.
Texte intégralMichigan. Office of the Auditor General. Audit report : Department of Labor financial and compliance audit, including the provisions of the Single Audit Act, October 1, 1984 through September 30, 1986. [Lansing, Mich.] (333 S. Capital Ave., Suite A, Lansing 48913) : State of Michigan, Office of the Auditor General, 1988.
Trouver le texte intégralKeller, Thomas. Use of fibre reinforced polymers in bridge construction. Zurich, Switzerland : International Association for Bridge and Structural Engineering (IABSE), 2003. http://dx.doi.org/10.2749/sed007.
Texte intégralGeneral, Michigan Office of the Auditor. Audit report : Financial audit, including the provisions of the Single Audit Act, of the Department of Mental Health, October 1, 1987 through September 30, 1989. [Lansing, Mich.] (201 N. Washington Square, Lansing 48913) : The Office, 1990.
Trouver le texte intégralMichigan. Office of the Auditor General. Audit report : Department of Management and Budget, financial and compliance audit, including the provisions of the Single Audit Act, October 1, 1984 through September 30, 1986. [Lansing, Mich.] (333 S. Capitol Ave., Suite A, Lansing 48913) : State of Michigan, Office of the Auditor General, 1988.
Trouver le texte intégralNew Jersey. Legislature. Joint Committee on the Public Schools. Committee meeting of Joint Committee on the Public Schools : Commissioner of Education, Dr. William Librera, will make a presentation of the New Jersey Quality Single Accountability Continuum proposal [June 17, 2004, Trenton, New Jersey]. Trenton, N.J : The Unit, 2004.
Trouver le texte intégralHenry H. Hayes Robert V. Dearing. Design and Test of a Small Single Stage Turbine. Creative Media Partners, LLC, 2021.
Trouver le texte intégralAn air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
Trouver le texte intégralInlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics. [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, 1999.
Trouver le texte intégralGC Works 1 : Single Stage Design and Build 1998 : Contract for Building and Civil Engineering Major Works - General Conditions. The Stationery Office Books (Agencies), 1998.
Trouver le texte intégralGeneral conditions of contract for building & civil engineering : Standard form of contract - single stage design & build version : GC/Works/1(Edition 3). HMSO, 1993.
Trouver le texte intégralThe 2006-2011 World Outlook for Multi-Stage Single-Or Double-Suction Diffuser-Design Radially Split Case Centrifugal Pumps with Discharge of 4 Inches or Less. Icon Group International, Inc., 2005.
Trouver le texte intégralParker, Philip M. The 2007-2012 World Outlook for Multi-Stage Single-Or Double-Suction Diffuser-Design Radially Split Case Centrifugal Pumps with Discharge of 4 Inches or Less. ICON Group International, Inc., 2006.
Trouver le texte intégralParker, Philip M. The 2007-2012 World Outlook for Multi-Stage Single-Or Double-Suction Volute-Or Diffuser-Design Axially Split Case Centrifugal Pumps with Discharge of over 8 Inches. ICON Group International, Inc., 2006.
Trouver le texte intégralThe 2006-2011 World Outlook for Multi-Stage Single-Or Double-Suction Volute-Or Diffuser-Design Axially Split Case Centrifugal Pumps with Discharge of over 8 Inches. Icon Group International, Inc., 2005.
Trouver le texte intégralThe 2006-2011 World Outlook for Multi-Stage Single-Or Double-Suction Volute-Or Diffuser-Design Axially Split Case Centrifugal Pumps with Discharge of 4 Inches or Less. Icon Group International, Inc., 2005.
Trouver le texte intégralParker, Philip M. The 2007-2012 World Outlook for Multi-Stage Single-Or Double-Suction Volute-Or Diffuser-Design Axially Split Case Centrifugal Pumps with Discharge of 4 Inches or Less. ICON Group International, Inc., 2006.
Trouver le texte intégralThe 2006-2011 World Outlook for Multi-Stage Single-Or Double-Suction Diffuser-Design Radially Split Case Centrifugal Pumps with Discharge of More Than 4 Inches and Up to 8 Inches. Icon Group International, Inc., 2005.
Trouver le texte intégralParker, Philip M. The 2007-2012 World Outlook for Multi-Stage Single-Or Double-Suction Diffuser-Design Radially Split Case Centrifugal Pumps with Discharge of More Than 4 Inches and Up to 8 Inches. ICON Group International, Inc., 2006.
Trouver le texte intégralSelection process for trade study : Graphite composite primary structure (GCPS). [Downey, Calif.] : Rockwell Aerospace, Space Systems Division, 1994.
Trouver le texte intégralAdvanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C : American Institute of Aeronautics and Astronautics, 1994.
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