A dual phase plane approach to the two-finite- burns minimum fuel rendezvous problem.
Two-finite burns minimum fuel rendezvous problem using dual phase plane description, determining control law
VARIATION METHOD↗
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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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A study of the application of microwave techniques to the measurement of solid propellant burning rates Progress report, 1 Sep. 1966 - 31 Aug. 1967
Microwave techniques for measurement of solid rocket propellant burning rates
Obrien, W. F., Jr.↗
An experimental investigation of near critical and supercritical burning of bipropellant droplets
High pressure combustion characteristics of single fuel droplet burning in air
Dominicis, D. P.↗
An Experimental Study of the Drag Coefficient of Burning Aluminum Droplets
Drag coefficient and Reynolds number of burning aluminum particles
Marshall, R. L.↗
Evolution of massive helium-burning supergiants.
Massive supergiant star models construction for core He plasma burning evolution phase, discussing luminosity and temperature sensitivity to internal instability
Chin, C.-W.↗
Predictions of burning times of metal particles.
Burning times for quasi-steady state combustion of spherical Al and Be particles, noting back diffusion of condensable gaseous combustion products and particle size effects
Kuehl, D. K.↗
A simple adaptive guidance scheme for minimum fuel two-finite-burns rendezvous.
Adaptive guidance scheme for minimum fuel two finite burns rendezvous from elliptical parking orbit to coplanar circular orbit
Trautwein, W.↗
An investigation of near critical and super- critical burning of fuel droplets Annual report, 1 Sep. 1967 - 1 Sep. 1968
Near critical and supercritical burning of fuel droplets
Faeth, G. M.↗
Two-burn escape maneuvers with an intermediate coasting ellipse
Two burn spacecraft trajectories for escaping earth parking orbit
Willis, E. A., Jr.↗
Experimental investigation of the effect of aluminum size and loading on the burning rate of solid propellants under acceleration
Aluminum size and loading effects on burning rate of centrifugal accelerated solid propellants
Jessee, W. P.↗
Rapid optimization of multiple-burn rocket flights, 8 March 1968 - 8 March 1969
Iterative solution of boundary value problem for rapid optimization of multiple-burn rocket flights
Brown, K. R.↗
Development of a hydrogen-burning annular combustor for use in a miniature gas turbine engine
Hydrogen burning annular combustor in miniature gas turbine engine for wind tunnel tests for obtaining aerodynamic characteristics
Burnett, M.↗
Nonlinear solid propellant burning rate behavior during abrupt pressure excursions.
Solid propellant burning rate behavior during abrupt environmental pressure excursions, using transient combustion model
Marxman, G. A.↗
Calculation of solid propellant burning rates from condensed-phase decomposition kinetics.
Solid propellant burning rates from condensed phase decomposition kinetics, discussing kinetic rates of thermal decomposition
Waesche, R. H. W.↗
Luminous fog layer surrounding a zirconium droplet burning in an oxygen-containing atmosphere.
Luminous spherical fog layer surrounding burning zirconium droplet during free fall through oxygen containing atmosphere, noting effect on mass and heat transfer processes
Marshall, R. L.↗
Transient burning of spherical symmetric fuel droplets.
Spherical symmetric unsteady conservation equations describing transient burning of volatile fuel droplets, obtaining time dependent fuel and heat distribution in flow field
Chervinsky, A.↗
Carbon-burning nucleosynthesis at constant temperature.
Elements nucleosynthesis during thermonuclear burning of carbon at series of temperatures and for several initial compositions
Arnett, W. D.↗
Remarks on extinguishment and the response function for a burning solid propellant.
Burning solid propellant behavior under pressure fluctuations expressed in response function terms defining small mass flux change ratio to small pressure change
Culick, F. E. C.↗