Space Programs Summary No. 37-43, Volume VI FOR the Period November 1, 1966 to December 31, 1966. Space Exploration Programs and Space Sciences
NASA space exploration programs design modifications and instrumentation developments
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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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NASA space exploration programs design modifications and instrumentation developments
Planning-Programming-Budgeting System /PPBS/ IMPLEMENTATION by Federal agencies and relation to space activities
Planning-Programming-Budgeting System /PPBS/ IMPLEMENTATION by Federal agencies and relation to space activities
Digital computer program for processing data of Explorer XVII voltage measurements of neutral atmospheric density and temperature
Space exploration programs and space science summary on Mariner, Ranger, and Surveyor projects - deep space instrumentation facility - environmental test facility
Computer program to select optical coating pattern for controlling temperature of spacecraft external surface
Computer program listing for selecting optical coating to control temperature of spacecraft external surface
Summary for research efforts for Surveyor project, Mariner program, Voyager project and Deep Space Network
Adaptation of field infrared terrain analysis spectral correlation program to IBM 7090 and recording tape voltage drift correction procedures
Orbital tracking program for analysis of data from C-band and S-band radar
The report summarizes DOE INFUSE-supported work between HB11 Energy and the University of Rochester’s TriForce Institute to improve computational modeling of advanced fusion fuels, especially proton–boron-11 (p- 11 B). The project extended the TriForce particle-in-cell/Monte Carlo collision code to include physics needed for dense, high-temperature p- 11 B burn studies, including p- 11 B fusion reactions, three-alpha-particle reaction products, relativistic Coulomb collisions, large-angle nuclear scattering, bremsstrahlung radiation, inverse bremsstrahlung absorption, and photon transport. The upgraded models were verified against focused physics tests and against known deuterium–tritium burn behavior. The study then used one-dimensional spherical simulations to estimate the conditions required for thermonuclear burn propagation in isochoric p- 11 B fuel. The calculations found that burn propagation is possible in the model, but only under very extreme hot-spot conditions, such as about 7000 g/cm 3 at 500 keV or 9000 g/cm 3 at 300 keV for a 20-micron hot spot. These conditions are much more demanding than current demonstrated inertial confinement fusion hot spots. The report concludes that the INFUSE collaboration successfully advanced kinetic and radiation modeling capabilities for p- 11 B fusion and provided useful estimates of ignition requirements. However, the simulated fuel gains remain below what would be needed for practical inertial fusion energy, and further work is needed to reconcile differences among kinetic, radiation-hydrodynamic, and analytic models and to identify more achievable target designs.
Reliability of sergeant missile assemblies - application of test-to-failure program
Fortran program using Monte Carlo method to establish probability distribution for rocket stage residual and total payload
Physiological parameter research and instrumentation development phases of long range program for in-flight monitoring in flight environment
Planning, programming, and budgeting system as aid to U.S. government agencies in management planning and decision making
Research program on management of research and development
Flowgraph construction, input-output formulation, and subroutines for Network Analysis for Systems Applications Program /NASAP/