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  • 1
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    Preliminary X-43 flight test results (2005)
    Elsevier
    Details
    Publication Date: 2005-07-01
    Print ISSN: 0094-5765
    Electronic ISSN: 1879-2030
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Elsevier
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    PAPER CURRENT
  • 2
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    Abort Flight Test Project Overview (2007)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: A general overview of the Orion abort flight test is presented. The contents include: 1) Abort Flight Test Project Overview; 2) DFRC Exploration Mission Directorate; 3) Abort Flight Test; 4) Flight Test Configurations; 5) Flight Test Vehicle Engineering Office; 6) DFRC FTA Scope; 7) Flight Test Operations; 8) DFRC Ops Support; 9) Launch Facilities; and 10) Scope of Launch Abort Flight Test
    Keywords: Aircraft Design, Testing and Performance
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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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
  • 4
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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 (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
  • 5
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    Initial flight qualification and operational maintenance of X-29A flight software (1989)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: A discussion is presented of some significant aspects of the initial flight qualification and operational maintenance of the flight control system softward for the X-29A technology demonstrator. Flight qualification and maintenance of complex, embedded flight control system software poses unique problems. The X-29A technology demonstrator aircraft has a digital flight control system which incorporates functions generally considered too complex for analog systems. Organizational responsibilities, software assurance issues, tools, and facilities are discussed.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-TM-101703 , H-1558 , NAS 1.15:101703 , AIAA PAPER 89-3596 , AIAA Guidance, Navigation and Control Conference; Aug 14, 1989 - Aug 16, 1989; Boston, MA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    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
  • 7
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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: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Flight control system design factors for applying automated testing techniques (1990)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Automated validation of flight-critical embedded systems is being done at ARC Dryden Flight Research Facility. The automated testing techniques are being used to perform closed-loop validation of man-rated flight control systems. The principal design features and operational experiences of the X-29 forward-swept-wing aircraft and F-18 High Alpha Research Vehicle (HARV) automated test systems are discussed. Operationally applying automated testing techniques has accentuated flight control system features that either help or hinder the application of these techniques. The paper also discusses flight control system features which foster the use of automated testing techniques.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA-TM-4242 , H-1631 , NAS 1.15:4242 , Annual Digital Avionics System Conference; Oct 15, 1990 - Oct 18, 1990; Virginia Beach, VA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 9
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    The F-18 systems research aircraft facility (1992)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: To help ensure that new aerospace initiatives rapidly transition to competitive U.S. technologies, NASA Dryden Flight Research Facility has dedicated a systems research aircraft facility. The primary goal is to accelerate the transition of new aerospace technologies to commercial, military, and space vehicles. Key technologies include more-electric aircraft concepts, fly-by-light systems, flush airdata systems, and advanced computer architectures. Future aircraft that will benefit are the high-speed civil transport and the National AeroSpace Plane. This paper describes the systems research aircraft flight research vehicle and outlines near-term programs.
    Keywords: RESEARCH AND SUPPORT FACILITIES (AIR)
    Type: NASA-TM-4433 , H-1844 , NAS 1.15:4433 , 1992 Aerotech Conference; Oct 05, 1992 - Oct 08, 1992; Anaheim, CA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    Flight control system design factors for applying automated testing techniques (1990)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The principal design features and operational experiences of the X-29 forward-swept-wing aircraft and F-18 high alpha research vehicle (HARV) automated test systems are discussed. It is noted that operational experiences in developing and using these automated testing techniques have highlighted the need for incorporating target system features to improve testability. Improved target system testability can be accomplished with the addition of nonreal-time and real-time features. Online access to target system implementation details, unobtrusive real-time access to internal user-selectable variables, and proper software instrumentation are all desirable features of the target system. Also, test system and target system design issues must be addressed during the early stages of the target system development. Processing speeds of up to 20 million instructions/s and the development of high-bandwidth reflective memory systems have improved the ability to integrate the target system and test system for the application of automated testing techniques. It is concluded that new methods of designing testability into the target systems are required.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: IEEE/AIAA/NASA Digital Avionics Systems Conference; Oct 15, 1990 - Oct 18, 1990; Virginia Beach, VA; United States
    Format: text
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    NASA TECHNICAL REPORTS
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