Книги з теми "Single stage design"
Оформте джерело за APA, MLA, Chicago, Harvard та іншими стилями
Ознайомтеся з топ-50 книг для дослідження на тему "Single stage design".
Біля кожної праці в переліку літератури доступна кнопка «Додати до бібліографії». Скористайтеся нею – і ми автоматично оформимо бібліографічне посилання на обрану працю в потрібному вам стилі цитування: APA, MLA, «Гарвард», «Чикаго», «Ванкувер» тощо.
Також ви можете завантажити повний текст наукової публікації у форматі «.pdf» та прочитати онлайн анотацію до роботи, якщо відповідні параметри наявні в метаданих.
Переглядайте книги для різних дисциплін та оформлюйте правильно вашу бібліографію.
American Institute of Aeronautics and Astronautics., Langley Research Center, and International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, Tenn.), eds. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.
Знайти повний текст джерелаAmerican Institute of Aeronautics and Astronautics. and International Aerospace Planes and Hypersonics Technologies Conference (6th : 1995 : Chattanooga, TN).), eds. Airbreathing/rocket single-stage-to-orbit design matrix. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. An air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Знайти повний текст джерелаMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Знайти повний текст джерелаMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Знайти повний текст джерелаMehta, Unmeel B. A two-stage-to-orbit spaceplane concept with growth potential. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 2001.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Requirements report for SSTO vertical take-off/horizontal landing vehicle. [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаOvtov, Vladimir. Machine parts. Course design. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1171976.
Повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. 1994 NASA/USRA/ADP design projects: Final report. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаCruse, Thomas. 1994 NASA/USRA/ADP design projects: Final report, NASw-4435. [Washington, DC: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Selection process for trade study: Reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Trade study plan for reusable hydrogen composite tank system (RHCTS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Test plans, GCPS task 4, subtask 4.2, thrust structure development. [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. 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.
Знайти повний текст джерелаH, Levack Daniel J., Nixon Robert F, and United States. National Aeronautics and Space Administration., eds. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерелаH, Levack Daniel J., Nixon Robert F, and United States. National Aeronautics and Space Administration., eds. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерелаH, Levack Daniel J., Nixon Robert F, and United States. National Aeronautics and Space Administration., eds. Advanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерелаGallaher, 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.
Знайти повний текст джерелаErich, Espenschied, Klop Jeffrey, and United States. National Aeronautics and Space Administration., eds. The control system for the X-33 linear aerospike engine. [Washington, DC: National Aeronautics and Space Administration, 1998.
Знайти повний текст джерелаErich, Espenschied, Klop Jeffrey, and United States. National Aeronautics and Space Administration., eds. The control system for the X-33 linear aerospike engine. [Washington, DC: National Aeronautics and Space Administration, 1998.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Milestone 4: Thrust structure concepts & IHM screening graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаNew 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.
Знайти повний текст джерелаMoseley, V. J. "Jon", Andreas Lampropoulos, Eftychia Apostolidi, and Christos Giarlelis. Characteristic Seismic Failures of Buildings. Edited by Stephanos E. Dritsos. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2019. http://dx.doi.org/10.2749/sed016.
Повний текст джерелаUrunov, Asror. Regional economy. ru: INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1013012.
Повний текст джерелаde 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.
Повний текст джерелаMichigan. 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.
Знайти повний текст джерелаKeller, 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.
Повний текст джерелаGeneral, 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.
Знайти повний текст джерелаMichigan. 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.
Знайти повний текст джерелаNew 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.
Знайти повний текст джерелаHenry H. Hayes Robert V. Dearing. Design and Test of a Small Single Stage Turbine. Creative Media Partners, LLC, 2021.
Знайти повний текст джерелаAn air-breathing launch vehicle concept for single-stage-to-orbit. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаInlet 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.
Знайти повний текст джерелаGC Works 1: Single Stage Design and Build 1998: Contract for Building and Civil Engineering Major Works - General Conditions. The Stationery Office Books (Agencies), 1998.
Знайти повний текст джерелаGeneral conditions of contract for building & civil engineering: Standard form of contract - single stage design & build version : GC/Works/1(Edition 3). HMSO, 1993.
Знайти повний текст джерелаThe 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.
Знайти повний текст джерелаParker, 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.
Знайти повний текст джерелаParker, 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.
Знайти повний текст джерелаThe 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.
Знайти повний текст джерелаThe 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.
Знайти повний текст джерелаParker, 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.
Знайти повний текст джерелаThe 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.
Знайти повний текст джерелаParker, 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.
Знайти повний текст джерелаSelection process for trade study: Graphite composite primary structure (GCPS). [Downey, Calif.]: Rockwell Aerospace, Space Systems Division, 1994.
Знайти повний текст джерелаAdvanced low-cost O₂/H₂ engines for the SSTO application. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерела