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title: 12th aiaa international space plants and hypersonic systems and technologies • title: 12th aiaa international space plane and hypersonic systems and technologies • title: 12th aiaa international space plates and hypersonic systems and technologies • title: 17th aiaa international space planes and hypersonic systems and technologies • title: 17th aiaa international space plants and hypersonic systems and technologies • title: 18th aiaa international space planes and hypersonic systems and technologies • title: 19th aiaa international space planes and hypersonic systems and technologies

Synonyme wurden verwendet für: Hypersonic • Space
Suche ohne Synonyme: title: 12th AIAA International Space Planes and Hypersonic Systems and Technologies

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    13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference. Flight Data Analysis of HyShot2

    N. E. Hass / M. K. Smart / A. Paull | NTIS | 2005
    The development of scramjet propulsion for alternative launch and payload delivery capabilities has comprised largely of ground experiments ...
    Verlag: National Aeronautics and Space Administration, Hampton, VA. Langley Research Center
    Schlagwörter: Space Technology

    Advanced Methods for Aircraft Engine Thrust and Noise Benefits: Nozzle-Inlet Flow Analysis

    Gilinsky, Mikhail / Morgan, Morris H. / Povitsky, Alex et al. | NTRS | 2001
    AIAA Paper #01-1893 has been accepted for the AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Propulsion And Power

    Aerosciences, Aero-Propulsion and Flight Mechanics Technology Development for NASA's Next Generation Launch Technology Program

    Cockrell, Charles E., Jr. | NTRS | 2003
    current design trade space includes rocket-propelled, hypersonic airbreathing and hybrid systems in two-stage and single-stage configurations ...
    Verlag: NASA National Aeronautics and Space Administration

    A Multifunctional Hot Structure Heatshield Concept for Planetary Entry

    Walker, Sandra P. / Daryabeigi, Kamran / Samareh, Jamshid A. et al. | NTRS | 2015
    material system has been evaluated for the load carrying structure, which will be utilized on the outer surface of the heatshield, and thus will ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance

    An Overview of NASA's Integrated Design and Engineering Analysis (IDEA) Environment

    Robinson, Jeffrey S. | NTRS | 2011
    true multi-disciplinary perspective, can the real performance benefits be achieved and complete vehicle systems be fielded. Toward this end ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    An Overview of the Role of Systems Analysis in NASA's Hypersonics Project

    Robinson, Jeffrey S. / Martin John G. / Bowles, Jeffrey V> et al. | NTRS | 2006
    Project with having a basic understanding of all systems that travel at hypersonic speeds within the Earth's and other planets atmospheres. This ...
    Verlag: NASA National Aeronautics and Space Administration

    A Technology Pathway for Airbreathing, Combined-Cycle, Horizontal Space Launch Through SR-71 Based Trajectory Modeling

    Kloesel, Kurt J. / Ratnayake, Nalin A. / Clark, Casie M. | NTRS | 2011
    made of the requisite research technology advances necessary for successful commercial and government adoption of combined-cycle engine systems ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Propulsion And Power

    Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

    Glass, David E. | NTRS | 2008
    Thermal protection systems (TPS) and hot structures are required for a range of hypersonic vehicles ranging from ballistic reentry to ...
    Verlag: NASA National Aeronautics and Space Administration

    Combustor Operability and Performance Verification for HIFiRE Flight 2

    Storch, Andrea M. / Bynum, Michael / Liu, Jiwen et al. | NTRS | 2011
    As part of the Hypersonic International Flight Research Experimentation (HIFiRE) Direct-Connect Rig (HDCR) test and analysis activity ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Fluid Mechanics And Thermodynamics

    Design Considerations of Istar Hydrocarbon Fueled Combustor Operating in Air Augmented Rocket, Ramjet and Scramjet Modes

    Andreadis, Dean / Drake, Alan / Garrett, Joseph L. et al. | NTRS | 2002
    The development and ground test of a rocket-based combined cycle (RBCC) propulsion system is being conducted as part of the NASA Marshall ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance

    Developing Optimized Trajectories Derived from Mission and Thermo-Structural Constraints

    Lear, Matthew H. / McGrath, Brian E. / Anderson, Michael P. et al. | NTRS | 2008
    In conjunction with NASA and the Department of Defense, the Johns Hopkins University Applied Physics Laboratory (JHU/APL) has been ...
    Verlag: NASA National Aeronautics and Space Administration

    Flight Data Analysis of HyShot 2

    Hass, Neal E. / Smart, Michael K. / Paull, Alan | NTRS | 2005
    The development of scramjet propulsion for alternative launch and payload delivery capabilities has comprised largely of ground experiments ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Spacecraft Design, Testing And Performance

    HIFiRE Direct-Connect Rig (HDCR) Phase I Scramjet Test Results from the NASA Langley Arc-Heated Scramjet Test Facility

    Cabell, Karen / Hass, Neal / Storch, Andrea et al. | NTRS | 2011
    Facility (AHSTF) at simulated Mach 8 flight conditions. These experiments were part of an initial test phase to support Flight 2 of the Hypersonic ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Fluid Mechanics And Thermodynamics

    Hypersonic Propulsion at Pratt and Whitney: Overview

    Kazmar, Richard R. | NTRS | 2002
    ) database was developed during the National Aero Space Plane (NASP) program using hydrogen fueled propulsion systems for space access vehicles and ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Propulsion And Power

    Hyper-X Engine Design and Ground Test Program

    Voland, R. T. / Rock, K. E. / Huebner, L. D. et al. | NTRS | 1998
    The Hyper-X Program, NASA's focused hypersonic technology program jointly run by NASA Langley and Dryden, is designed to move hypersonic ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Hyper-X Mach 7 Scramjet Design, Ground Test and Flight Results

    Ferlemann, Shelly M. / McClinton, Charles R. / Rock, Ken E. et al. | NTRS | 2005
    of the airframe integrated scramjet engine. This flight was a crucial first step toward realizing the potential for airbreathing hypersonic ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Fluid Mechanics And Thermodynamics

    Hyper-X Stage Separation: Simulation Development and Results

    Reubush, David E. / Martin, John G. / Robinson, Jeffrey S. et al. | NTRS | 2001
    This paper provides an overview of stage separation simulation development and results for NASA's Hyper-X program; a focused hypersonic ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Investigation of REST-Class Hypersonic Inlet Designs

    Gollan, Rowan / Ferlemann, Paul G. | NTRS | 2011
    Rectangular-to-elliptical shape-transition (REST) inlets are of interest for use on scramjet engines because they are efficient and ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Fluid Mechanics And Thermodynamics

    Materials Development for Hypersonic Flight Vehicles

    Glass, David E. / Dirling, Ray / Croop, Harold et al. | NTRS | 2006
    Materials Integrated Product Team (MIPT) was formed to lead the development of key thermal protection system (TPS) and hot structures technologies ...
    Verlag: NASA National Aeronautics and Space Administration

    NASA Hypersonics Overview

    Charles P Leonard | NTRS
    Verlag: NASA National Aeronautics and Space Administration

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