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    HYPERVELOCITY STAGNATION POINT HEAT TRANSFER IN A CARBON DIOXIDE ATMOSPHERE

    GRABER, B. C. / MORGAN, C. J. / NEREM, R. M. | AIAA | 1963

    PREFERRED SCHEMES FOR MULTIPLE ORBIT TRANSFER

    BILLIK, B. H. / PRICE, C. M. | AIAA | 1963

    APPROXIMATE BURST STRENGTH OF THIN-WALLED CYLINDERS WITH HEMISPHERICAL CAPS

    COSTANTINO, C. J. / SALMON, M. A. / WEIL, N. A. | AIAA | 1963

    HIGH SPEED SCANNER FOR TRANSVERSE RADIATION MEASUREMENTS OF LUMINOUS HYPERSONIC WAKES

    CARBONE, R. M. / KECK, J. C. / MELCHER, B. W. et al. | AIAA | 1963

    Electrogasdynamic power generation

    GOURDINE, M. C. / KAHN, B. | AIAA | 1964

    A method of calculating rocket plume radiation to the base region

    ABU-ROMIA, M. M. / TIEN, C. L. | AIAA | 1964

    Hall-current accelerator utilizing surface contact ionization

    BANAS, C. M. / BROWN, C. O. / PINSLEY, E. A. | AIAA | 1964

    Experimental results in high-specific-impulse thermoionic acceleration

    DUCATI, A. C. / GIANNINI, G. M. / MUEHLBERGER, E. | AIAA | 1964

    Influence of stress history on time-dependent spall in metals

    BARKER, L. M. / BUTCHER, B. M. / LUNDERGAN, C. D. et al. | AIAA | 1964

    Operational planning for general aviation facilities at airports

    BURNS, H. C. / WARSKOW, M. A. | AIAA | 1964

    Operational flight control for saturn boost vehicles

    FILIAS, G. / PESANDO, M. / STEEG, C. W. | AIAA | 1964

    Photomicrography of electrically sprayed heavy particles

    CARSON, R. S. / HENDRICKS, C. D. / HOGAN, J. J. et al. | AIAA | 1964

    Factors influencing electrically sprayed liquids

    CARSON, R. S. / HENDRICKS, C. D. / HOGAN, J. J. et al. | AIAA | 1964

    An investigation of hall propulsor characteristics

    BRANDMAIER, H. E. / DURAND, J. L. / GOURDINE, M. C. et al. | AIAA | 1964

    Vstol development of the c-130 hercules

    DANSBY, T. / GARRARD, W. C. J. / RYLE, D. M. et al. | AIAA | 1964

    Temperature measurement in a chemical shock tube by sodium-line reversal and c sub 2 reversal methods

    NAPIER, D. H. / NETTLETON, M. / SIMONSON, J. R. et al. | AIAA | 1964

    Experiment in solar orientation of spin stabilized satellite

    CROCKER, M. C. / VRABLIK, E. A. | AIAA | 1965

    Ignition of an evaporating fuel in a hot, stagnant gas containing an oxidizer

    HERMANCE, C. E. / SHINNAR, R. / SUMMERFIELD, M. | AIAA | 1965

    Design and operating considerations of commercial stol transports

    DECKERT, W. H. / HOLZHAUSER, C. A. / KELLY, M. W. et al. | AIAA | 1965

    Ignition and combustion of aluminum in small- scale liquid rocket engines

    DEAN, L. E. / KEITH, R. C. / SUMNER, T. L. et al. | AIAA | 1965

    Physical property distributions in a low- pressure crossed-field plasma accelerator.

    DENISON, M. R. / DUCLOS, D. P. / WU, Y. C. L. et al. | AIAA | 1965

    On predicting thermal conductivity of a binary mixture of solids.

    FOSTER, J. M. / SMITH, C. B. / VACHON, R. I. | AIAA | 1966

    Elastomeric thermal shield systems for lifting reentry vehicles.

    CLINE, P. P. / DOLAN, C. M. / EDIGHOFFER, H. H. et al. | AIAA | 1966

    Dynamic stability of cylindrical shells.

    BIENIEK, M. P. | AIAA | 1966

    Combustion system for an underwater thermal propulsion system.

    CARAHER, J. M. / JACKLEY, D. N. | AIAA | 1966