Książki na temat „Single stage design”
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American Institute of Aeronautics and Astronautics., Langley Research Center i International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, Tenn.), red. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.
Znajdź pełny tekst źródłaAmerican Institute of Aeronautics and Astronautics. i International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, TN).), red. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.
Znajdź pełny tekst źródłaCenter, NASA Glenn Research, red. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaCenter, NASA Glenn Research, red. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaCenter, NASA Glenn Research, red. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Znajdź pełny tekst źródłaMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Znajdź pełny tekst źródłaMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Znajdź pełny tekst źródłaMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Requirements report for SSTO vertical take-off/horizontal landing vehicle. [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaOvtov, Vladimir. Machine parts. Course design. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1171976.
Pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 1994 NASA/USRA/ADP design projects: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaCruse, Thomas. 1994 NASA/USRA/ADP design projects: Final report, NASw-4435. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Selection process for trade study: Reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Trade study plan for reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Test plans, GCPS task 4, subtask 4.2, thrust structure development. [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. 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.
Znajdź pełny tekst źródłaH, Levack Daniel J., Nixon Robert F i United States. National Aeronautics and Space Administration., red. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Znajdź pełny tekst źródłaH, Levack Daniel J., Nixon Robert F i United States. National Aeronautics and Space Administration., red. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Znajdź pełny tekst źródłaH, Levack Daniel J., Nixon Robert F i United States. National Aeronautics and Space Administration., red. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Znajdź pełny tekst źródłaGallaher, 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.
Znajdź pełny tekst źródłaErich, Espenschied, Klop Jeffrey i United States. National Aeronautics and Space Administration., red. The control system for the X-33 linear aerospike engine. [Washington, DC: National Aeronautics and Space Administration, 1998.
Znajdź pełny tekst źródłaErich, Espenschied, Klop Jeffrey i United States. National Aeronautics and Space Administration., red. The control system for the X-33 linear aerospike engine. [Washington, DC: National Aeronautics and Space Administration, 1998.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaNew 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.
Znajdź pełny tekst źródłaMoseley, V. J. "Jon", Andreas Lampropoulos, Eftychia Apostolidi i Christos Giarlelis. Characteristic Seismic Failures of Buildings. Redaktor Stephanos E. Dritsos. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2019. http://dx.doi.org/10.2749/sed016.
Pełny tekst źródłaUrunov, Asror. Regional economy. ru: INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1013012.
Pełny tekst źródłade 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.
Pełny tekst źródłaMichigan. 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.
Znajdź pełny tekst źródłaKeller, 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.
Pełny tekst źródłaGeneral, 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.
Znajdź pełny tekst źródłaMichigan. 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.
Znajdź pełny tekst źródłaNew 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.
Znajdź pełny tekst źródłaHenry H. Hayes Robert V. Dearing. Design and Test of a Small Single Stage Turbine. Creative Media Partners, LLC, 2021.
Znajdź pełny tekst źródłaAn air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Znajdź pełny tekst źródłaInlet 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.
Znajdź pełny tekst źródłaGC Works 1: Single Stage Design and Build 1998: Contract for Building and Civil Engineering Major Works - General Conditions. The Stationery Office Books (Agencies), 1998.
Znajdź pełny tekst źródłaGeneral conditions of contract for building & civil engineering: Standard form of contract - single stage design & build version : GC/Works/1(Edition 3). HMSO, 1993.
Znajdź pełny tekst źródłaThe 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.
Znajdź pełny tekst źródłaParker, 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.
Znajdź pełny tekst źródłaParker, 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.
Znajdź pełny tekst źródłaThe 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.
Znajdź pełny tekst źródłaThe 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.
Znajdź pełny tekst źródłaParker, 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.
Znajdź pełny tekst źródłaThe 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.
Znajdź pełny tekst źródłaParker, 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.
Znajdź pełny tekst źródłaSelection process for trade study: Graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Znajdź pełny tekst źródłaAdvanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Znajdź pełny tekst źródła