A statistical loads study of S-IC control engine-out conditions on the Apollo Saturn 5 vehicle
Monte Carlo method for S-IC control engine-out condition study on Saturn 5 launch vehicle
Meadows, M. T.↗
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Results for “Monte Carlo method”
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 brief discussion of Berger's latest Monte Carlo program
Computer program based on Monte Carlo method for calculating transport of electrons and photons through matter
Derrickson, J. H.↗
Hybrid computer optimization of systems with random parameters
Hybrid computer Monte Carlo method for optimization of systems containing random parameters
White, R. C., Jr.↗
Simulating the consequence of cloud cover on earth-viewing space missions
Cloud cover consequence on earth photographing space missions simulated by Monte Carlo method using worldwide statistics
Brown, S. C.↗
Chain-pooling ANOVA for two-level factorial replication-free experiments
Chain pooling tests for two level factorial replication-free experiments using Monte Carlo methods
Berrettoni, J. N.↗
A Monte Carlo technique for determining sphere drag in near free molecular flow
First collision Monte Carlo method for calculating aerodynamic drag on hard sphere and Maxwell molecular models in near-free molecular flow
Robertson, S. J.↗
Simulation of the nuclear-electromagnetic cascade development in an ionization spectrometer
Longitudinal nuclear-electromagnetic cascade in ionization spectrometer simulated by Monte Carlo method, noting energy relationship to particle sum recording
Jones, W. V.↗
Monte Carlo modeling of the Martian atmosphere from Viking mission design point of view
Martian atmosphere modeling for obtaining Viking lander spacecraft design margins by Monte Carlo method
Mukhopadhyay, A. K.↗
Electron impact excitation of N2
Molecular nitrogen excitation under electron bombardment at auroral and airglow impact levels, using computerized Monte Carlo method
Brinkmann, R. T.↗
Energy deposition by auroral electrons in the atmosphere
Spatial distribution of energy deposited by auroral electrons in upper atmosphere, using Monte Carlo method
Berger, M. J.↗
A preliminary Monte-Carlo analysis of the reflection of an imploding hemispherical shock wave similar to that generated in the UTIAS implosion driven hypervelocity launcher or shock tube
Cold wall and multibody collision effects on reflection of imploding shock waves using Monte Carlo method and molecular dynamics
Macpherson, A. K.↗
Study of the modulatory effects of the solar wind on galactic cosmic rays
Mathematical model using Monte Carlo method for modulation of galactic protons by solar wind
Moss, T. A.↗
Implications of regolith thickness in the Apollo 16 landing site
Determining thickness of regolith in Apollo 16 landing site by Monte Carlo method
Oberbeck, V. R.↗
Probable solar flare doses encountered on an interplanetary mission as calculated by the MCFLARE code
Probable solar flare doses on interplanetary mission calculated by MCFLARE computer program using Monte Carlo methods
Karp, I. M.↗
Diffuse reflection from clouds with horizontal inhomogeneities
Diffuse reflection from clouds with horizontal surface striations, using Monte Carlo method to follow photons through simplified models
Van Blerkom, D. J.↗
The modulation of galactic protons by the solar wind - A Monte Carlo approach
Solar wind modulation effects on galactic protons and cosmic rays, using radial magnetic field mathematical model and Monte Carlo method
Giuli, R. T.↗
Probable solar flare doses encountered on an interplanetary mission as calculated by the MCFLARE code
The computer program, MCFLARE, uses Monte Carlo methods to simulate solar flare occurrences during an interplanetary space voyage. The total biological dose inside a shielded crew compartment due to the flares encountered during the voyage is determined. The computer program evaluates the doses obtained on a large number of trips having identical trajectories. From these results, a dose D sub p having a probability p of not being exceeded during the voyage can be determined as a function of p for any shield material configuration. To illustrate the use of the code, a trip to Mars and return is calculated, and estimated doses behind several thicknesses of aluminum shield and water shield are presented.
Lahti, G. P.↗
Nuclear radiation environment analysis for thermoelectric outer planet spacecraft
Neutron and gamma ray transport calculations were performed using Monte Carlo methods and a three-dimensional geometric model of the spacecraft. The results are compared with similar calculations performed for an earlier design.
Davis, H. S.↗