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Source: The Open Library

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1High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)

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“High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)” Metadata:

  • Title: ➤  High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)
  • Author:
  • Language: English
  • Number of Pages: Median: 537
  • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast
  • Publish Date:

“High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1991
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

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2Air-breathing aerospace plane development essential

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“Air-breathing aerospace plane development essential” Metadata:

  • Title: ➤  Air-breathing aerospace plane development essential
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

“Air-breathing aerospace plane development essential” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1994
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    3CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system

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    “CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Metadata:

    • Title: ➤  CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Springfield, Va

    “CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1997
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

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      4Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation

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      “Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation” Metadata:

      • Title: ➤  Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation
      • Author:
      • Language: English
      • Number of Pages: Median: 41
      • Publisher: ➤  Ames Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - [For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va - Washington, D.C

      “Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1990
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

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        5Design and evaluation of candidate pressure ports for the HYFLITE experiment

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        “Design and evaluation of candidate pressure ports for the HYFLITE experiment” Metadata:

        • Title: ➤  Design and evaluation of candidate pressure ports for the HYFLITE experiment
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Design and evaluation of candidate pressure ports for the HYFLITE experiment” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1994
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

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          6Particle kinetic simulation of high altitude hypervelocity flight

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          “Particle kinetic simulation of high altitude hypervelocity flight” Metadata:

          • Title: ➤  Particle kinetic simulation of high altitude hypervelocity flight
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - NASA National Aeronautics and Space Administration, Ames Research Center
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Springfield, Va - [Washington, DC - [Moffett Field, Calif.]

          “Particle kinetic simulation of high altitude hypervelocity flight” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1994
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

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            7CFD for hypersonic propulsion

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            “CFD for hypersonic propulsion” Metadata:

            • Title: CFD for hypersonic propulsion
            • Author:
            • Language: English
            • Publisher: Lewis Research Center
            • Publish Date:
            • Publish Location: [Cleveland, Ohio

            “CFD for hypersonic propulsion” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1991
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

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              8Propulsion over a wide Mach number range

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              “Propulsion over a wide Mach number range” Metadata:

              • Title: ➤  Propulsion over a wide Mach number range
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Cornell University
              • Publish Date:
              • Publish Location: ➤  Ithaca, NY - Springfield, Va - [Washington, DC

              “Propulsion over a wide Mach number range” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1989
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

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                9Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30

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                “Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30” Metadata:

                • Title: ➤  Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30
                • Author:
                • Number of Pages: Median: 13
                • Publisher: ➤  American Institute of Aeronautics and Astronautics
                • Publish Date:
                • Publish Location: Washington, D. C

                “Compressible laminar boundary layers for perfect and real gases in equilibrium at Mach numbers to 30” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1992
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                10Investigation of piloting aids for manual control of hypersonic maneuvers

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                “Investigation of piloting aids for manual control of hypersonic maneuvers” Metadata:

                • Title: ➤  Investigation of piloting aids for manual control of hypersonic maneuvers
                • Author:
                • Language: English
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va - [Springfield, Va

                “Investigation of piloting aids for manual control of hypersonic maneuvers” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1995
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

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                  11Improving the performance of two-stage gas guns by adding a diaphragm in the pump tube

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                  “Improving the performance of two-stage gas guns by adding a diaphragm in the pump tube” Metadata:

                  • Title: ➤  Improving the performance of two-stage gas guns by adding a diaphragm in the pump tube
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - [Washington, DC

                  “Improving the performance of two-stage gas guns by adding a diaphragm in the pump tube” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1995
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                    12[Nonlinear issues in the aerothermochemistry of gases and materials and the associated physics and dynamics of interfaces]

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                    “[Nonlinear issues in the aerothermochemistry of gases and materials and the associated physics and dynamics of interfaces]” Metadata:

                    • Title: ➤  [Nonlinear issues in the aerothermochemistry of gases and materials and the associated physics and dynamics of interfaces]
                    • Author:
                    • Language: English
                    • Publisher: ➤  Florida A&M University, Laboratory for Modern Fluid Physics - National Aeronautics and Space Administration - National Technical Information Service, distributor
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - [Washington, DC - Tallahassee, Fla

                    “[Nonlinear issues in the aerothermochemistry of gases and materials and the associated physics and dynamics of interfaces]” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1996
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

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                      13Vehicle integration effects on hypersonic waveriders

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                      “Vehicle integration effects on hypersonic waveriders” Metadata:

                      • Title: ➤  Vehicle integration effects on hypersonic waveriders
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                      “Vehicle integration effects on hypersonic waveriders” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1994
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

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                        14Transpiration cooling in hypersonic flight

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                        “Transpiration cooling in hypersonic flight” Metadata:

                        • Title: ➤  Transpiration cooling in hypersonic flight
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                        “Transpiration cooling in hypersonic flight” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1989
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

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                          15Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment

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                          “Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment” Metadata:

                          • Title: ➤  Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                          • Publish Date:
                          • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                          “Hypersonic engine leading edge experiments in a high heat flux, supersonic flow environment” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1994
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Access

                          Downloads Are Not Available:

                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                            16Hypersonic vehicle model and control law development using H and u synthesis

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                            “Hypersonic vehicle model and control law development using H and u synthesis” Metadata:

                            • Title: ➤  Hypersonic vehicle model and control law development using H and u synthesis
                            • Author:
                            • Number of Pages: Median: 35
                            • Publisher: Langley Research Center
                            • Publish Date:
                            • Publish Location: Hampton, Va

                            “Hypersonic vehicle model and control law development using H and u synthesis” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1994
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            17Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment

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                            “Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment” Metadata:

                            • Title: ➤  Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                            • Publish Date:
                            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                            “Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1994
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

                            Downloads Are Not Available:

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                              18Application of computational fluid dynamics in high speed aeropropulsion

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                              “Application of computational fluid dynamics in high speed aeropropulsion” Metadata:

                              • Title: ➤  Application of computational fluid dynamics in high speed aeropropulsion
                              • Author:
                              • Language: English
                              • Publisher: Lewis Research Center
                              • Publish Date:
                              • Publish Location: [Cleveland, Ohio

                              “Application of computational fluid dynamics in high speed aeropropulsion” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1991
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

                              Online Access

                              Downloads Are Not Available:

                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                                19One-dimensional modeling of hypersonic flight propulsion engines

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                                “One-dimensional modeling of hypersonic flight propulsion engines” Metadata:

                                • Title: ➤  One-dimensional modeling of hypersonic flight propulsion engines
                                • Author:
                                • Publisher: AIAA
                                • Publish Date:
                                • Publish Location: Washington, D. C

                                “One-dimensional modeling of hypersonic flight propulsion engines” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1989
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                20Combined cycle propulsion for hypersonic flight

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                                “Combined cycle propulsion for hypersonic flight” Metadata:

                                • Title: ➤  Combined cycle propulsion for hypersonic flight
                                • Author:
                                • Number of Pages: Median: 10
                                • Publisher: AIAA
                                • Publish Date:
                                • Publish Location: New York

                                “Combined cycle propulsion for hypersonic flight” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1987
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                21Propulsion challenges of hypersonic flight

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                                “Propulsion challenges of hypersonic flight” Metadata:

                                • Title: ➤  Propulsion challenges of hypersonic flight
                                • Author:
                                • Publisher: AIAA
                                • Publish Date:
                                • Publish Location: New York

                                “Propulsion challenges of hypersonic flight” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1986
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                22Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit

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                                “Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit” Metadata:

                                • Title: ➤  Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit
                                • Author:
                                • Number of Pages: Median: 18
                                • Publisher: ➤  Institute for Aerospace Studies
                                • Publish Date:
                                • Publish Location: [Downsview, Ont.]

                                “Non-linear effects in the longitudinal dynamics of a lifting vehicle in a circular orbit” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1960
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                Wiki

                                Source: Wikipedia

                                Wikipedia Results

                                Search Results from Wikipedia

                                Hypersonic flight

                                Hypersonic flight is flight through the atmosphere below altitudes of about 90 km (56 mi) at speeds greater than Mach 5, a speed where dissociation of

                                Hypersonic weapon

                                A hypersonic weapon is a weapon that can travel and maneuver significantly during atmospheric flight at hypersonic speed, which is defined as above Mach

                                Hypersonic Technology Vehicle 2

                                unmanned hypersonic bomber aircraft. The DARPA/AF Falcon Hypersonic Technology Vehicle (HTV) demonstration program was designed to enable the in-flight demonstration

                                Hypersonic speed

                                In aerodynamics, hypersonic speed refers to speeds much faster than the speed of sound, usually more than approximately Mach 5. The precise Mach number

                                DARPA Falcon Project

                                second phase of the Hypersonic Weapon System development was to perform a set of flight tests with a series of boost-glide Hypersonic Technology Vehicles

                                Long-Range Hypersonic Weapon

                                The Long-Range Hypersonic Weapon (LRHW), also known as the Dark Eagle, is an intermediate-range surface-to-surface boost-glide hypersonic weapon being developed

                                Hypersonic glide vehicle

                                The in-flight maneuverability of HGVs makes them unpredictable, allowing them to effectively evade air defenses. As of 2022[update], hypersonic glide vehicles

                                Boeing X-51 Waverider

                                Waverider is an unmanned research scramjet experimental aircraft for hypersonic flight at Mach 5 (3,300 mph; 5,300 km/h) and an altitude of 70,000 feet (21

                                Hypersonic Air-breathing Weapon Concept

                                Advanced Research Projects Agency (DARPA), that had a successful hypersonic flight announced in September 2021. It is a kinetic energy weapon, without

                                Scaled Composites Stratolaunch

                                air-launch-to-orbit (ALTO) rockets, and subsequently repurposed to offer air launch hypersonic flight testing after a change of ownership. It was announced in December


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