Radiation effects testing of Saturn telemetry hardware
Radiation effects testing of Saturn telemetry hardware
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Radiation effects testing of Saturn telemetry hardware
Hardware-software provisions for multiple precision floating point arithmetic
Low thrust mission simulation dependence on hardware definition, discussing power plant characteristics, jet velocity and thrustor efficiency
Side wall currents in unignited hardware type thermionic energy converters, discussing work function and heat choke
Leak detection for aerospace hardware, discussing equipment, operations, checkout, etc
Computer memory reduction through Fortran higher level language, discussing tradeoff between costs saved and additional logic hardware
Unified hardware-software design for digital computers
Hardware and software requirements for propulsion flight analysis computers
Hardware requirements for space shuttle cryogenic systems
Probability density function of hardware performance parameter and incentive contracting
Hardware and system testing mathematical model assuming stochastic design and manufacturing defects detection and nondetection probability equations analogous to reliability function
Apollo command and service modules environmental control system, discussing redesign of faulty hardware
Low thrust mission simulation dependence on hardware definition, discussing power plant characteristics, jet velocity and thrustor efficiency
Apollo J mission hardware modification for lunar exploration, describing systems engineering role
Integrated Life Support System hardware tests, discussing oxygen and water recovery, contaminant control, personal accommodations and failure detection
Computer memory reduction through Fortran higher level language, discussing tradeoff between costs saved and additional logic hardware
The hardware for the technical feasibility demonstration models for weightlessness analysis was improved, and a 60-day test was conducted. The results are presented in detail.
A market survey and evaluation of inertial guidance systems (inertial measurement units and digital computers) were made. Comparisons were made to determine the candidate systems for use in the Scout launch vehicle. Error analyses were made using typical Scout trajectories. A reaction control system was sized for the fourth stage. The guidance hardware to Scout vehicle interface was listed.