A review of shock waves around aeroassisted orbital transfer vehicles
暂无分享,去创建一个
[1] G. Menees,et al. Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept , 1985 .
[2] C. B. Davies,et al. Aerodynamics of generalized bent biconics for aero-assisted, orbital-transfer vehicles , 1985 .
[3] G. Walberg. A Survey of Aeroassisted Orbit Transfer , 1985 .
[4] John M. Beggs,et al. Space station - The next logical step , 1984 .
[5] S. Garland,et al. Integration becomes the name of the OTV game , 1984 .
[6] D. Desautel. Analytical characterization of AOTV perigee aerothermodynamic regime. [Aeroassisted Orbital Transfer Vehicle] , 1984 .
[7] R. C. Ried,et al. An AOTV aeroheating and thermal protection study , 1984 .
[8] John T. Howe,et al. Introductory Aerothermodynamics of Advanced Space Transportation Systems , 1983 .
[9] H. Goldstein,et al. Developments in fibrous refractory composite insulation , 1980 .
[10] D. Nestler,et al. DEVELOPMENT OF AN AFTERBODY RADIATIVE AND CONVECTIVE HEATING CODE FOR OUTER PLANET PROBES , 1978 .
[11] Charles E. Rose,et al. Flight characteristics of probes in the atmospheres of Mars, Venus and the outer planets☆ , 1977 .
[12] J. Arnold,et al. Composition of the earth's atmosphere by shock-layer radiometry during the PAET entry probe experiment. , 1973 .
[13] James O. Arnold,et al. Nonequilibrium effects on shock-layer radiometry during earth entry. , 1973 .
[14] W. L. Jones,et al. Theoretical and measured electron-density distributions for the ram vehicle at high altitudes. , 1972 .
[15] W. D. Goodrich,et al. The aerothermodynamic environment of the Apollo command module during superorbital entry , 1972 .
[16] J. P. Appleton,et al. Excitation Mechanisms of the Nitrogen Frist‐Positive and First‐Negative Radiation at High Temperature , 1972 .
[17] Sangwook Kang. Nonequilibrium, Ionized, Hypersonic Flow over a Blunt Body at Low Reynolds Number , 1970 .
[18] C. J. Schexnayder,et al. Computation of ionization in re-entry flowfields , 1970 .
[19] Jr. J. C. Adams. Shock slip analysis of merged layer stagnation point air ionization , 1970 .
[20] G. C. Lyle,et al. A computer program for a line-by-line calculation of spectra from diatomic molecules and atoms assuming a Voight line profile , 1969 .
[21] R. Nerem,et al. An analysis of re-entry flight measurements of shock layer microwaveradiation , 1969 .
[22] C. Park,et al. On convergence of computation of chemically reacting flows , 1985 .
[23] J. J. Rehder,et al. Multiple-pass trajectories for an aeroassisted orbital transfer vehicle , 1984 .
[24] P. Shih,et al. Low Lift-to-Drag Aerobrake Heat-Transfer Test at Mach 10 , 1984 .
[25] C. Park,et al. Shock-tube studies of radiative base heating of Jovian probe , 1980 .
[26] C. Park. Modeling of radiative heating of base region of Jovian entry probe , 1979 .
[27] Graeme A. Bird,et al. Molecular Gas Dynamics , 1976 .
[28] V. J. Scullin,et al. General chemical kinetics computer program for static and flow reactions, with application to combustion and shock-tube kinetics , 1972 .
[29] Dean R. Chapman,et al. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition , 1958 .
[30] Fred T. Jane,et al. All the world's aircraft , 1914 .