1–10 of 13 hits
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    INSAT-2A and 2B development mechanisms

    Sathyanarayan, M. N. / Rao, M. Nageswara / Nataraju, B. S. et al. | NTRS | 1994

    Comparison of FDNS liquid rocket engine plume computations with SPF/2

    Kumar, G. N. / Griffith, D. O., II / Warsi, S. A. et al. | NTRS | 1993

    Hybrid combustion with metallized fuels

    Yi, Jianwen / Wygle, Brian S. / Bates, Ronald W. et al. | NTRS | 1993

    Minimum fuel spacecraft reorientation

    Seywald, H. / Kumar, R. R. / Deshpande, S. M. et al. | NTRS | 1992

    COBE ground segment attitude determination

    Kumar, V. K. / Freedman, I. / Wright, E. L. et al. | NTRS | 1991

    COBE ground segment gyro calibration

    Freedman, I. / Kumar, V. K. / Rae, A. et al. | NTRS | 1991

    Object oriented fault diagnosis system for space shuttle main engine redlines

    Rogers, John S. / Mohapatra, Saroj Kumar | NTRS | 1990

    A study of time dissemination via satellite in India

    Mathur, B. S. / Banerjee, P. / Sood, P. C. et al. | NTRS | 1979