1–10 von 37 Ergebnissen
|

    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