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  • 2000-2004  (5)
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  • 1
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    Hyper-X Program Status (2001)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper provides an overview of the objectives and status of the Hyper-X program, which is tailored to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment. The first Hyper-X research vehicle (HXRV), designated X-43. is being prepared at the Dryden Flight Research Center for flight at Mach 7. Extensive risk reduction activities for the first flight are completed, and non-recurring design activities for the Mach 10 X-43 (3rd flight) are nearing completion. The Mach 7 flight of the X-43, in the spring of 2001, will be the first flight of an airframe-integrated scramjet-powered vehicle. The Hyper-X program is continuing to plan follow-on activities to focus an orderly continuation of hypersonic technology development through flight research.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper 2001-0828 , Aerospace Sciences; Jan 08, 2001 - Jan 12, 2001; Reno, NV; United States
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Unknown
    Hyper-X Program Status (2001)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper provides an overview of the objectives and status of the Hyper-X program, which is tailored to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment. The first Hyper-X research vehicle (HXRV), designated X-43, is being prepared at the Dryden Flight Research Center for flight at Mach 7. Extensive risk reduction activities for the first flight are completed, and non-recurring design activities for the Mach 10 X-43 (third flight) are nearing completion. The Mach 7 flight of the X-43, in the spring of 2001, will be the first flight of an airframe-integrated scramjet-powered vehicle. The Hyper-X program is continuing to plan follow-on activities to focus an orderly continuation of hypersonic technology development through flight research.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper 2001-1910 , 10th International Space Planes and Hypersonic Systems and Technologies Conference Committee; Apr 24, 2000 - Apr 27, 2000; Kyoto; Japan
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Unknown
    The Aircraft Simulation Role in Improving Flight Safety Through Control Room Training (2002)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: NASA Dryden Flight Research Center uses its six-degrees-of-freedom (6-DOF) fixed-base simulations for mission control room training to improve flight safety and operations. This concept is applied to numerous flight projects such as the F-18 High Alpha Research Vehicle (HARV), the F-15 Intelligent Flight Control System (IFCS), the X-38 Actuator Control Test (XACT), and X-43A (Hyper-X). The Dryden 6-DOF simulations are typically used through various stages of a project, from design to ground tests. The roles of these simulations have expanded to support control room training, reinforcing flight safety by building control room staff proficiency. Real-time telemetry, radar, and video data are generated from flight vehicle simulation models. These data are used to drive the control room displays. Nominal static values are used to complete information where appropriate. Audio communication is also an integral part of training sessions. This simulation capability is used to train control room personnel and flight crew for nominal missions and emergency situations. Such training sessions are also opportunities to refine flight cards and control room display pages, exercise emergency procedures, and practice control room setup for the day of flight. This paper describes this technology as it is used in the X-43A and F-15 IFCS and XACT projects.
    Keywords: Aircraft Design, Testing and Performance
    Type: NASA/TM-2002-210731 , H-2501 , NAS 1.15:210731 , AIAA Modeling and Simulation Technologies Conference; Aug 05, 2002 - Aug 08, 2002; Monterey, CA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
    facet.materialart.
    Unknown
    Hyper-X Program Status (2001)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper provides an overview of the objectives and status of the Hyper-X program, which is tailored to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment. The first Hyper-X research vehicle (HXRV), designated X-43, is being prepared at the Dryden Flight Research Center for flight at Mach 7. Extensive risk reduction activities for the first flight are completed, and non-recurring design activities for the Mach 10 X-43 (3rd flight) are nearing completion. The Mach 7 flight of the X-43, in the spring of 2001, will be the first flight of an airframe-integrated scramjet-powered vehicle. The Hyper-X program is continuing to plan follow-on activities to focus an orderly continuation of hypersonic technology development through flight research.
    Keywords: Aircraft Design, Testing and Performance
    Type: AIAA Paper 2001-0828 , Aerospace Sciences; Jan 08, 2001 - Jan 12, 2001; Reno, NV; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 5
    facet.materialart.
    Unknown
    NASA's Hyper-X Program (2000)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper provides an overview of the objectives and status of the Hyper-X program which is tailored to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment, the last stage preceding prototype development. The first Hyper-X research vehicle (HXRV), designated X-43, is being prepared at the Dryden Flight Research Center for flight at Mach 7 in the near future. In addition, the associated booster and vehicle-to-booster adapter are being prepared for flight and flight test preparations are well underway. Extensive risk reduction activities for the first flight and non-recurring design for the Mach 10 X-43 (3rd flight) are nearing completion. The Mach 7 flight of the X-43 will be the first flight of an airframe-integrated scramjet-powered vehicle.
    Keywords: Aircraft Design, Testing and Performance
    Type: IAF Paper 00-V.4.01 , 51st International Astronautical Congress; Oct 02, 2000 - Oct 06, 2000; Rio de Janeiro; Brazil
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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