Solid Propellant Combustion Diagnostic Techniques
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Solid Propellant↗
Engineering topics
Strand, Leon D.
Publications and source records attributed to Strand, Leon D..
Extended Duty Cycle Testing of Spacecraft Propulsion Miniaturized Components
The object of this study was to assess the functional performance of prototype miniaturized
Miniaturized↗
Characterization of Hybrid Rocket Internal Heat Flux and HTPB Fuel Pyrolysis
None given. From statement of problem:The broad nature of this work has been to extend our understanding of the nature of the conventional or classical hybrid rocket combustion process (fuel decomposition, heat and mass transfer, and chemical reaction), and the critical engineering parameters that define this process.
rocket↗
Study Of Fuels For Hybrid Rockets
Report describes experimental study of combustion and rates of regression of selected fuels for hybrid rocket engines. Part of continuing effort to develop fuels with greater rates of regression and lesser dependence on shapes of fuel grains and to maximize potential specific impulse at low cost.
Strand, Leon D.↗
Hybrid Propulsion Based on Fluid-Controlled Solid Gas Generators
The use of fuel-rich solid (gas generator-type) propellants for hybrid propulsion affords some design and utilization efficiency advantages. Both forward and aft liquid injection control concepts are evaluated form the operational standpoints of ballistics, throttling, Stability and extinguishment.
Propulsion↗
Hybrid propulsion based on fluid-controlled solid gas generators
The use of fuel-rich solid (gas generator-type) propellants for hybrid propulsion affords some design and utilization efficiency advantages. Both forward and aft liquid injection control concepts are evaluated from the operational standpoints of ballistics, throttling, stability and extinguishment. Steady-state and non-steady ballistics analyses are employed for this evaluation. Stability of solid motor operation is enhanced by fluid injection with adequate injector pressure drop. Efficient throttling and reliable extinguishment are attained through a combination of solid propellant combustion tailoring, grain design, control valves and sensors. Initial results from a laboratory-scale slab combustor, combining a gas generator propellant with gaseous oxygen injection, are also presented.
Cohen, Norman S.↗
Measuring Response Of Propellant To Oscillatory Heat Flux
Apparatus for research in combustion of solid propellants measures oscillatory response of rate of burning to oscillating thermal radiation from modulated CO2 laser. Determines response to rate of burning to equivalent oscillation in pressure. Rod of propellant mounted in burner assembly including waveguide at one end and infrared window at other end. Microwave Doppler velocimeter measures motion of combustion front. Microwave, laser-current, and heat-flux signals processed into and recorded in forms useful in determining desired response of propellent.
Strand, Leon D.↗