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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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Consistent field Monte Carlo method calculation for collision effect on electron-ion diode characteristics and for hard sphere electron- neutral collision effect for monoenergetic- thermionic emission
Monte Carlo method for determination of touchdown dynamics for soft lunar landing
Hybrid analog-digital computer systems for Monte Carlo method applications
Monte Carlo analysis of rarefied-gas heat transfer between parallel plates under various flow conditions
Monte Carlo method for computing Atlas/Centaur flight performance reserve
Monte Carlo computer program for transmission probability for gas molecular flow through two coaxial cylinders in series
Radiative heat transfer calculations by Monte Carlo method
Computer program for evaluating flight performance reserve requirements for Centaur vehicle using Monte Carlo method
Monte Carlo method to predict solid propellant variability effects on Algol ID motor performance, for Little Joe II project
Monte Carlo analysis of sphere transmission experiments for average capture cross sections from slow neutron resonance spectroscopy data
Monte Carlo codes for IBM 7090 digital computer to calculate radiation heating in propellant tanks, and radiation environment about nuclear rocket stage
Couette flow and heat transfer between parallel plates enclosing hard-sphere rarefied gas analyzed by Monte Carlo method
N-body Monte Carlo simulation of specific lunar orbiter missions
Radiative heat transfer calculated by Monte Carlo method
Consistent-field Monte Carlo method used to calculate electron and ion diode characteristics, including effect of collisions
Steady flow of highly rarefied ionized gas through channel with magnetic field solved by Monte Carlo method obtaining density, energies, wall shear stress, etc
Couette flow and heat transfer through hard- sphere rarefied gas enclosed between parallel walls analyzed by Monte Carlo method
Monte Carlo simulation for adaptive policy for multiple impulse correction of trajectory of spacecraft