Development of the post-injection propulsion system for the Mariner C spacecraft
Monopropellant hydrazine-fueled rocket used as post injection propulsion system for Mariner C spacecraft
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Monopropellant hydrazine-fueled rocket used as post injection propulsion system for Mariner C spacecraft
Impulsive injection of electrons into earths inner trapping region from solar cosmic ray events
Refraction of injected point source of sound by cold nitrogen jet, noting effects of temperature and velocity fields
Digital computer program calculates the cooling effectiveness and flow characteristics resulting from the mixing of a cool liquid injectant /water/ with a hot sonic or subsonic gas stream /hydrogen/. The output of the program provides pressure, temperature, velocity, density, composition, and Mach number profiles at any location in the mixing duct.
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Gaseous film cooling of rocket motor with injection near throat
Apparatus, techniques, and instrumentation for experimental correlation of nonreactive injection schemes and combustion effects in liquid propellant rocket engine
Plasma injection from coaxial gun into magnetic trap with opposite fields
Nitrogen injection effects on boundary layer of graphite surface in high-temperature dissociated airflow
Injection of drag reducing fluid into turbulent pipe flow of Newtonian fluid
Heat shield efficiency over plane surface during injection through two tangential slots studied in wind tunnel
Syringe injection system for seeding plasma with Na-K alloy in study of MHD power generation and propulsion
Range capability of gallium arsenide injection LIDAR against extended targets and corner reflectors under both negligible and high background radiation conditions
Statistical techniques for missile injection error analysis, discussing direct and adjoint methods
Mass injection effect on compressible three- dimensional laminar boundary layers analyzed for nonreacting gas, using conservation equations for flow velocity profiles
Staged vortex amplifier with integral gas generators for liquid rocket secondary injection thrust vector control
Approximation method for calculating heat, and mass exchange in laminar multicomponent boundary layer near stagnation point of injected gases
Liquid surface profile determination in cryogenic tank during gas injection