A forecast of space technology. Part 2: Management of information
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Engineering topics
Publications and source records attributed to Dipprey, D. F..
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A brief overview of the state of knowledge in liquid rocket technology is presented and examples are provided of instances where some fundamental principles of chemistry, fluid mechanics, and mathematics can be applied. A liquid propellant rocket classification is discussed together with rocket system performance, applications for liquid propellants, the effective exhaust velocity, aspects of simplified nozzle expansion, questions about theoretical propellant performance, the effect of chamber pressure on equilibrium performance, and the kinetic recombination in nozzles. Details of propellant combustion are examined, giving attention to propellant injection, evaporation-controlled combustion, combustion instability, and monopropellant decomposition.
Mars and Venus atmospheres as working fluids in gas turbines and liquid oxidizers for rocket engines
Use of earth-storable propellants in unmanned spacecraft propulsion systems for flights to near planets and moon
Earth storable propellants exist in liquid phase in near-Earth temperatures at vapor pressure below 100 psi and hypergolic, yielding simple, reliable and predictable systems
Relationship between heat transfer and friction in smooth and rough tubes