ROCKET ENGINE STARTING WITH MIXED OXIDES OF NITROGEN AND LIQUID AMMONIA BY FLOW-LINE ADDITIVES
Rocket engine starting with mixed oxides of nitrogen and liquid ammonia by flow-line additives
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Rocket engine starting with mixed oxides of nitrogen and liquid ammonia by flow-line additives
Low-temperature chemical starting of combined jp-4 nitric acid propellant for low-thrust rocket engine using three-fluid propellant valve
Injector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia
Experimental effect of gas flow transients on heat emission of burning liquid drops in a rocket combustor
Attenuation of tangent-pressure oscillation in liquid-oxygen-heptane rocket engine combustion chamber using longitudinal fin
Satellite instrumentation tested aboard a sounding rocket - atmospheric drag tests
Space science - step rocket optimization theory
Ultraviolet stellar spectra from rocket soundings, comparison of observed radiation flux with model stellar atmospheres and interstellar radiation
Structural analysis of upper atmosphere from rocket and satellite measurements of charged particles
Liquid dynamics in rocket propellant tanks
High altitude sounding rockets for upper air temperature and density measurements
Mechanical impedance study of the x-259 rocket engine
Optimal rocket flight in gravitation field
Selection of thrust chamber cooling technique for liquid propelled spacecraft rocket engines
Scale model testing of 90-deg turn ejector systems for rocket engine simulation
Gaseous phase of detonation - relation to rocket propulsion
Hot kerosene flashing in vertical tube - simulation of flow pattern of phase-change rocket combustor
Theoretical models and experimental rocket combustors for study of combustion process instability