Supercritical burning of liquid droplets in stagnant environment.
Supercritical burning of liquid fuel droplets in stagnant environment, using flame sheet model to obtain heat and mass fields
Chervinsky, A.↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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The effect of atmosphere selection and gravity on burning rate and ignition temperature
Atmospheric selection and gravity effects on burning rate and ignition temperature
Colombo, G. V.↗
A physical model for downward burning
Elementary physical model for flammable materials combustion emphasizing downward burning
Adelberg, M.↗
A Study of the Results of Tests Investigating the Effect of Acceleration and Gas Composition on the Burning Rate of Spacecraft Materials
Effects of acceleration and gas composition on burning rate of spacecraft materials
Adelberg, M.↗
A study of the results of tests investigating the effect of acceleration on the burning rate of spacecraft materials
Effects of acceleration on burning rate of spacecraft materials
Adelberg, M.↗
Bipropellant droplet burning rates and lifetimes in a combustion gas environment
Liquid rocket propellant droplet burning rate and lifetimes in combustion chamber
Faeth, G. M.↗
An investigation of near critical and super- critical burning of fuel droplets Annual report, 1 Sep. 1968 - 31 Dec. 1969
Experimental droplet burning rates obtained at atmospheric pressure in combustion gas environment
Faeth, G. M.↗
Stability limits and efficiency of swirl-can combustor modules burning natural gas fuel
Stability limits and efficiency of swirl can combustor modules burning natural gas fuel
Marchionna, N. R.↗
Finite and impulsive burn simulations of fixed-attitude translunar injection aborts. Project Apollo
Finite and impulsive burn simulations of fixed attitude translunar injection aborts
Foggatt, C. E.↗
Feasibility of manual completion of a LOI burn. Volume 1 - IMU drift about the pitch axis
Manual completion of lunar orbit insertion burn with inertial measuring unit drifting about pitch axis
Treadway, A. H.↗
Feasibility of manual completion of a LOI burn. Volume 2 - BMAG drift about the pitch axis. Project Apollo
Feasibility of manual completion of LOI burn with body mounted attitude gyro drifting about pitch axis
Treadway, A. H.↗
Burning of solid aluminum and magnesium spheres in high-temperature and high-velocity gases
Burning solid aluminum and magnesium spheres in high temperature and high velocity gases by combustion of hydrogen and oxygen
Ingebo, R. D.↗
A technique for controlling the position of a burning solid-propellant sample in a combustion bomb
Position control of burning solid nonmetallized propellant strand in combustion bomb using closed loop servomechanism
Derr, R. L.↗
Scanning electron microscopy of BeO whiskers formed on the surface of burning beryllium droplets
BeO whiskers formation on burning Be droplets surface using scanning electron microscopy, noting temperature effects
Prentice, J. L.↗
Rapid optimization of multiple-burn rocket flights
Shooting method for real time optimization of multiple burn rocket flights, presenting analysis, algorithm and test results
Brown, K. R.↗
Effects of the acceleration vector on transient burning-rate augmentation of an aluminized solid propellant
Aluminized solid propellant transient burning rate augmentation during acceleration loads
Northam, G. B.↗
Role of scanning electron microscopy in the study of solid propellant combustion. III - The surface structure and profile characteristics of burning composite solid propellants
Composite solid propellants surface structure and profile characteristics burning with various oxidizers and polyurethane binder by scanning electron microscopy
Boggs, T. L.↗
A study of the application of microwave techniques to the measurement of solid propellant burning rates Final report
Utilization of Doppler microwave interferometer for measuring solid propellant burning rates
Wood, H. L.↗