Project gemini design integration.
Project objectives effect on design philosophy and specific considerations for Gemini two man spacecraft
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Project objectives effect on design philosophy and specific considerations for Gemini two man spacecraft
Test program philosophy of electric propulsion and power for planetary mission application
This is Volume I of a two-volume work on the theory, of phase-locked receivers, with pertinent reference material on practical receiver design. Volume I is primarily devoted to the performance of carrier-tracking loops, including a rigorous treatment of narrow-band systems having IF limiters. The bulk of the work is based on a theoretical linear model, but a nonlinear method is also presented to predict behavior near the threshold. The emphasis throughout the work is toward completeness, simplicity, and internal consistency of the material assembled. Part I of this Volume is an exposition of the theory, the resulting equations, and the design philosophy that have enabled the phase-lock concept to evolve into the basic principle underlying the most sensitive receivers il, the world today. Part II is a condensed version of Part I, intended as a quick reference to formulas, definitions, and salient design considerations.
Reliability measures and management philosophies in development of Gemini launch vehicle
Test program philosophy of electric propulsion and power for planetary mission application
Mariner 1964 parts screening program including philosophy, program implementation, screening results and conclusions
Philosophy, purpose, and effectiveness of unmanned environment simulation in ground tests of spacecraft reliability
Physiological monitoring applied to man in space environment, emphasizing overall philosophy including need and results of monitoring
This paper discusses the ground control and monitoring function performed in support of the Gemini rendezvous missions. Included are discussions of the support philosophy adopted for Gemini; the resulting influence upon mission design; and comparisons between predicted and actual flight results.
Design philosophy for cost reductions on future space transportation systems, exemplifying application to booster system for earth orbital logistics
Design philosophy and checkout procedure of Cassegrain-Coude telescope
Philosophy and technology of unmanned spacecraft sterilization and planetary quarantine
Range safety philosophy and practice concerning malfunctioning missile and space vehicle launch and flight
Survey of management abstracts including subject categories in contract, personnel, program, and project management, research and development, tools, techniques, and philosophy of management
Influence of advanced technology and design philosophies on general aviation aircraft for 1985
Data bus for avionics system of space shuttle, noting functions of interface unit, error detection and recovery, redundancy, and bus control philosophy
ATM for manned solar observation, discussing thermal design, thermal vacuum test philosophy, mathematical models and analytical and test data correlation