Performance analysis of Open MPI on AMR applications over Slingshot-11
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97 MATHEMATICS AND COMPUTING↗
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Results for “performance analysis”
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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Agent Path Optimizations with PADL on 2D Grids: Behavioral Analysis, Performance Metrics, and Stability Considerations
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Demireva, Maria [Lawrence Livermore National Labor↗
A PERFORMANCE ANALYSIS OF ELECTRICAL PROPULSION SYSTEMS
Space science - electric propulsion systems for space vehicles
SPACE VEHICLE↗
PERFORMANCE ANALYSIS OF HIGH-ENERGY CHEMICAL STAGES FOR INTERPLANETARY MISSIONS. PART III- BRAKE TO MARS ORBIT
Chemical propulsion for interplanetary flight and design of spacecraft for braking into orbit around planet mars
MARS /PLANET/↗
Performance analysis of chemical stages in the 300 to 400 second specific impulse range for interplanetary missions
Trajectory parameters for escaping from & braking into earth orbit utilizing single vehicle stage with high specific impulse
SPECIFIC IMPULSE↗
Monte carlo performance analysis computer program with programmed mixture ratio
Fortran program using Monte Carlo method to establish probability distribution for rocket stage residual and total payload
FORTRAN↗
Manned space flight network performance analysis for the sa-8 mission
Orbital mission of Pegasus B payload with Apollo boilerplate spacecraft, launched by Saturn SA-8 - summary
PEGASUS SATELLITE↗
Performance analysis of chemical stages in the 300 to 400 second specific impulse range for interplanetary missions
Effect of thrust-weight ratios and specific impulses on trajectory parameters for earth orbit hyperbolic escape and entry
TRAJECTORY ANALYSIS↗
Materials manual for use with TRW space radiator-condenser design and performance analysis computer programs
Thermophysical properties of working fluids and tube, header, and fin materials and compatibility analysis for design of space electric power radiator-condenser systems
CONDENSER RADIATOR↗
Performance Analysis of Composite Propulsion Systems, Phase 1 Final Report, 30 Dec. 1966 - 29 Dec. 1967
Design and fabrication of combustion and test stand for evaluating composite propulsion system
Wrubel, J. A.↗
Performance analysis of PCM signal conditioners incorporating an advanced technique in testing procedures.
PCM synchronizer testing providing processing and print-out for Apollo checkout equipment
Cooner, C. E.↗
AC-16 final guidance equations and performance analysis
AC-16 guidance equations for OAO-A2 mission
Seiley, R. E.↗
Performance analysis of an infrared pilot- warning indicator system
Optical IR system as low cost pilot warning indicator providing audible and visual collision warnings to general aviation aircraft
Leigh, C. H.↗
Mission analysis performance parameters for 1978-1980 Jovian probe oriented missions
Jovian probe and spacecraft mission feasibility, discussing launch opportunities, targeting, objectives and data transmission
Fields, D. P.↗
Solid Rocket Motor Performance Analysis and Prediction
Current design practices are reviewed and assessed, and guidance is established for achieving greater consistency in design, reliability in the end product, and efficiency in the design effort. The total problem is discussed, and design elements involved in successful design are identified. Design criteria are described, and the rule, guide, limitation, or standard which must be imposed on each essential design element is given. Recommended practices are presented for satisfying each of the criteria.
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Development and performance analysis of a trajectory estimator for an entry through the Martian atmosphere.
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Jones, J. F.↗
Performance Analysis and Design Synthesis (PADS) computer program. Volume 1: Formulation
The program formulation for PADS computer program is presented. It can size launch vehicles in conjunction with calculus-of-variations optimal trajectories and can also be used as a general-purpose branched trajectory optimization program. In the former use, it has the Space Shuttle Synthesis Program as well as a simplified stage weight module for optimally sizing manned recoverable launch vehicles. For trajectory optimization alone or with sizing, PADS has two trajectory modules. The first trajectory module uses the method of steepest descent; the second employs the method of quasilinearization, which requires a starting solution from the first trajectory module.
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Thermoelectric pump performance analysis computer code
A computer program is presented that was used to analyze and design dual-throat electromagnetic dc conduction pumps for the 5-kwe ZrH reactor thermoelectric system. In addition to a listing of the code and corresponding identification of symbols, the bases for this analytical model are provided.
Johnson, J. L.↗