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Synonyme wurden verwendet für: Performance: • Research • Research Center
Suche ohne Synonyme: title: NASA. Langley Research Center Shuttle Performance: Lessons Learned, Part 1

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    Shuttle Performance: lessons learned : Proceedings of a Conference / J. P. Arrington; J. J. Jones [Hrsg.]. NASA Langley Research Center ; 1

    NASA Langley Research Center | TIBKAT | 1983

    Space shuttle orbiter venting: Lessons learned

    Lutfi, H. S. / Nieder, R. L. | NTRS | 1983
    Shuttle orbiter. Good correlation has been obtained between predicted and measured compartment pressures during the orbital flight test (OFT ...
    Verlag: NASA National Aeronautics and Space Administration

    Space shuttle launch vehicle aerodynamic uncertainties: Lessons learned

    Hamilton, J. T. | NTRS | 1983
    presented. Comparisons of and conclusions drawn from flight minus predicted data and uncertainties are given. Lessons learned from the Space Shuttle ...
    Verlag: NASA National Aeronautics and Space Administration

    Explanation of the hypersonic longitudinal stability problem: Lessons learned

    Griffith, B. J. / Maus, J. R. / Best, J. T. | NTRS | 1983
    Inviscid and viscous CFD codes have been applied to a modified Space Shuttle orbiter geometry to investigate differences between preflight ...
    Verlag: NASA National Aeronautics and Space Administration

    Lessons learned for composite structures

    Whitehead, R. S. | NTRS | 1991
    significant factor in overall part cost, and improved batch-to-batch pre-preg physical property control. Historical manufacturing lessons learned are ...
    Verlag: NASA National Aeronautics and Space Administration

    Approach and landing characteristics of the space shuttle orbiter Learned, Pt. 1 p 637-651

    Bourne, C. A. / Kirsten, P. W. | NTRS | 1983
    The first five Space Shuttle orbiter landng during the Orbital Flight Test program are analyzed with respect to the unique requirement to ...
    Verlag: NASA National Aeronautics and Space Administration

    Space shuttle descent flight control design requirements and experiments Learned, Pt. 1 p 617-628

    Kafer, G. / Wilson, D. | NTRS | 1983
    Some of the lessons learned during the development of the Space Shuttle descent flight control system (FCS) are reviewed. Examples confirm ...
    Verlag: NASA National Aeronautics and Space Administration

    Shuttle booster separation aerodynamics

    Craig, M. K. / Dresser, H. S. | NTRS | 1983
    A wind tunnel test program of some complexity was used to define the aerodynamic forces exerted on the space shuttle solid rocket boosters ...
    Verlag: NASA National Aeronautics and Space Administration

    Space shuttle entry longitudinal aerodynamic comparisons of flights 1-4 with preflight predictions

    Romere, P. O. / Whitnah, A. M. | NTRS | 1983
    The Space Shuttle orbiter flight test program has required the aerodynamicist to take a new approach in determining flight characteristics ...
    Verlag: NASA National Aeronautics and Space Administration

    Shuttle launch debris: Sources, consequences, solutions

    Craig, M. K. | NTRS | 1983
    Following the first space shuttle flight, the shuttle program established a team to identify and eliminate sources of debris which had ...
    Verlag: NASA National Aeronautics and Space Administration

    Shuttle ascent GN&C postflight results

    Mcswain, G. | NTRS | 1983
    the Space Transportation System 1 flight. The lessons learned from the orbital flight test program are being used to enhance the overall ...
    Verlag: NASA National Aeronautics and Space Administration

    Ascent air data system results from the space shuttle flight test program

    Hillje, E. R. / Nelson, R. L. | NTRS | 1983
    air data system performance met the user requirements. Lessons learned are enumerated, the most important being the need for a thorough ...
    Verlag: NASA National Aeronautics and Space Administration

    Development of space shuttle ignition overpressure environment and correlation with flight data

    Lai, S. | NTRS | 1983
    rocket motors (SRM's) is one of the critical design factors assessed for lift-off. The STS-1 ignition overpressure design environment was ...
    Verlag: NASA National Aeronautics and Space Administration

    Predicted and flight test results of the performance, stability and control of the space shuttle from reentry to landing

    Kirsten, P. W. / Richardson, D. F. / Wilson, C. M. | NTRS | 1983
    Aerodynaic performance, stability and control data obtained from the first five reentries of the Space Shuttle orbiter are given. Flight ...
    Verlag: NASA National Aeronautics and Space Administration

    Techniques for assessment of ascent aerodynamic characteristics of the space shuttle launch system

    Leahy, K. S. | NTRS | 1983
    In order to investigate the impact of ascent element aerodynamics on the flight constraints of the Space Shuttle, a system of programs was ...
    Verlag: NASA National Aeronautics and Space Administration

    Aerodynamic analysis of the loft anomaly observed on orbital flight tests of the space shuttle

    Surber, T. E. / Stone, J. S. | NTRS | 1983
    The loft anomaly observed during the launch phase of the orbital flight tests (OFT) of the Space Shuttle is described and evidence that the ...
    Verlag: NASA National Aeronautics and Space Administration

    Minimum testing of the space shuttle orbiter for stability and control derivatives

    Cooke, D. R. | NTRS | 1983
    A unique approach has been developed for stability and control derivative testing of the Space Shuttle orbiter during entry. Shuttle ...
    Verlag: NASA National Aeronautics and Space Administration

    Space shuttle orbiter reaction control subsystem flight data anomalies

    Stone, J. S. / Baumbach, J. J. / Roberts, B. B. | NTRS | 1983
    Shuttle orbiter vehicle flight data obtained during operation of the reaction control subsystem (RCS) were compared with predictions ...
    Verlag: NASA National Aeronautics and Space Administration

    Approach to establishing the effect of aeroelasticity on aerodynamic characteristics of the space shuttle orbiter

    Schlosser, D. C. / Dominik, D. F. | NTRS | 1983
    ) Space Shuttle orbiter were estimated by a simplified approach called the elevon torsional stiffness (ETS) method. This method employs rigid ...
    Verlag: NASA National Aeronautics and Space Administration

    Calculation of Shuttle Base Heating Environments and Comparison with Flight Data

    Greenwood, T. F. / Lee, Y. C. / Bender, R. L. et al. | NTRS | 1983
    The techniques, analytical tools, and experimental programs used initially to generate and later to improve and validate the Shuttle base ...
    Verlag: NASA National Aeronautics and Space Administration

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