Aeronautics & Astronautics - Fluid & Thermal Sciences > Rocket Propulsion: Page 2

No. 29040 Maximum missile velocity vs different mass ratios No. 29041 Drag coefficient vs Mach number for a V-2 rocket missile No. 29042 Lift coefficient vs Mach number for V-2 rocket missile No. 29043 Free-body force diagram with wings and fins No. 29044 Simplified free-body force diagram without wings and fins No. 29045 Flight path for a simple single-stage rocket No. 29046 Planetary exploration vehicle with two stages No. 29047 Various orbital parameters of a space vehicle as function of altitude No. 29048 Interplanetary mission typical powered-flight maneuvers No. 29049 Elliptical orbit No. 29050 Elliptical free-flight trajectory for a long-range ballistic missile No. 29051 Unguided nonmaneuvering air-launched rocket projectile trajectory No. 29052 Liquid oxygen and hydrocarbon fuel performance characteristics No. 29053 Liquid oxygen and hydrocarbon fuel chamber gas composition No. 29054 Specific impulse as a function of pressure & mixture ratios No. 29055 Enthalpy and entropy as function of mixture ratio in rocket propellant No. 29056 Parameter variation with pressure ratio: hydrocarbon-oxygen propellant No. 29057 Exhaust gas composition variation at nozzle exit No. 29058 Liquid propellant rocket feed system classifications No. 29059 Turbopump feed system: gas generator cycle No. 29060 Turbopump feed system: staged-combustion cycle No. 29061 Tandem tanks with external piping: turbopump-fed rocket engine No. 29062 Tandem tanks with internal piping: Turbopump-fed rocket engines No. 29063 Concentric tanks: Turbopump-fed rocket engines No. 29064 Top view of multi-tank rocket engine No. 29065 Multi-tank: Turbopump-fed rocket engines No. 29066 Pressure profile as a function of time for a pulsing rocket engine No. 29067 Adiabatic reaction temp. vs Ammonia decomposition: Hydrazine reactor No. 29068 Characteristic velocity vs Ammonia decomposition: Hydrazine reactor No. 29069 Specific impulse vs Ammonia decomposition: Hydrazine reactor No. 29070 Average molecular weight vs Ammonia decomposition: Hydrazine reactor No. 29071 Molar composition vs Ammonia decomposition: Hydrazine reactor No. 29072 Typical oscillogram trace for smooth combustion in a rocket No. 29073 Typical oscillogram trace for rough combustion in a rocket No. 29074 Typical oscillogram trace for unsteady combustion in a rocket No. 29077 Thrust chamber inner wall: Typical stresses No. 29078 Doublet impinging stream pattern of an injector No. 29079 Triplet impinging stream pattern of an injector No. 29080 Self-impinging stream pattern of an injector No. 29081 Shower head stream pattern of an injector No. 29082 Hollow post and sleeve element of an injector No. 29083 Variable injection area concentric tube injector No. 29084 Hydraulic characteristics plots for four types of injector orifices No. 29085 Injection orifice type No. 29086 Injector orifice No. 29087 Type of injector orifice No. 29088 Four kinds of injector orifices' hydraulic characteristics No. 29089 Orifice with sharp edges No. 29090 Orifice with a short tube and rounded entrance No. 29091 Orifice with a short tube and conical entrance
 

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