Electromagnetic compatibility testing
Electromagnetic compatibility acceptance tests for Saturn S-IC stages
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Electromagnetic compatibility acceptance tests for Saturn S-IC stages
Computer-controlled launch set design and feasibility for checkout and launching of Centaur guidance system
Launch automation programs for Saturn IB SYSTEM utilizing digital computer techniques to increase vehicle reliability from manufacturing through prelaunch checkout
Ground checkout and prelaunch testing of Gemini spacecraft - launch site operations
Checkout functions for onboard testing of Saturn instrument unit and S-IVB stages, and implementation guidelines for incorporation into space vehicle system
Multiparameter monitoring visual displays for Apollo prelaunch checkout
Flight checkout system breadboard design, construction and testing
Compatibility of checkout systems for rockets and space vehicles, with application to Saturn V launch vehicle
Aerospace vehicle simulation concept defined, examining relation to major problem areas of checkout
Analysis and projections of space vehicle automatic checkout and launch
Man-rated space simulation facility, emphasizing checkout and qualification of systems
Self-contained and vehicle integrated on-board checkout systems, considering controller-evaluator and sensors
Leak detection for aerospace hardware, discussing equipment, operations, checkout, etc
Leak detection for aerospace hardware, discussing equipment, operations, checkout, etc
A program plan for system evaluation of the two-dimensional Scanning Laser Doppler System (SLDS) is presented. In order to meet system evaluation and optimization objectives the following tests were conducted: (1) noise tests; (2) wind tests; (3) blower flowfield tests; (4) single unit (1-D) flyby tests; and (5) dual unit (2-D) flyby tests. Test results are reported. The final phase of the program included logistics preparation, equipment interface checkouts, and data processing. It is concluded that the SLDS is capable of accurately tracking aircraft wake vortices from small or large aircraft, and in any type of weather.
Apollo-Saturn program automatic checkout systems, discussing ground support equipment facility automation, computer software and checkout technique applications to nuclear electronic systems
Shuttle related considerations (constraints and guidelines) are compiled for use by designers of a potential class of large space structures which are transported to orbit and, deployed, fabricated or assembled in space using the Space Shuttle Orbiter. Considerations of all phases of shuttle operations from launch to ground turnaround operations are presented. Design of large space structures includes design of special construction fixtures and support equipment, special stowage cradles or pallets, special checkout maintenance, and monitoring equipment, and planning for packaging into the orbiter of all additional provisions and supplies chargeable to payload. Checklists of design issues, Shuttle capabilities constraints and guidelines, as well as general explanatory material and references to source documents are included.
Automation techniques for stage checkout in Saturn program noting equipment, time factor, etc