Simulator study of a turn procedure for reducing airspace requirements for supersonic transports
Computer simulation study of turn procedure for reducing airspace requirements for supersonic transports
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Computer simulation study of turn procedure for reducing airspace requirements for supersonic transports
Lower bound procedure for energy eigenvalues and helium ground state calculations
Manual procedure for determining position in space from onboard optical measurements - celestial navigation
Program analysis and evaluation procedures for alternative space program planning
Test procedures for reliability of electronic components in nuclear radiation environment
Application of numerical integration procedures to restricted three-body problem
Temperature correction procedure for atmosphere model calculation
Electronic instrumentation and procedures for environmental and reliability testing of UK-2/S-52 international satellite
Diagnostic monitoring in office procedures - biotelemetry
Space radiation effects on Apollo mission - operational procedures for dose reduction
Standard test procedures for initiators of explosive devices
Ion engine subsystem reliability procedure based on safety-factor number obtained from stress analysis
Reliability procedure involving stress analysis and safety factor number determination applied to ion engine subsystem
Computational procedure reduces the numerical effort whenever the method of finite differences is used to solve ablation problems for which the surface recession is large relative to the initial slab thickness. The number of numerical operations required for a given maximum space mesh size is reduced.
Narrow-gap welding procedures for joining thick gauge aluminum alloy plate
Optimal procedures for stochastically failing equipment
Sequential ranking procedures, stochastic processes, and statistical analysis