Real time space vehicle and ground support systems software simulator for launch programs checkout
Real time simulation of space vehicle and ground support equipment by digital computer for launch programs checkout
Brown, P. A.↗
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Results for “Checkout”
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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Developments in automatic checkout of manned space vehicles
Onboard automatic checkout systems for manned space vehicles, investigating data management development costs for thorough tradeoff studies
Vavra, P. H.↗
Selecting and sequencing tests in adaptive checkout processes
Test selecting and sequencing for adaptive checkout processes, determining malfunctions
Wollmer, R. D.↗
Survey of automatic checkout systems for Saturn V stages
NASA automatic checkout systems for Saturn 5 stages and instrument units
Schmidt, D. M.↗
Electronic checkout system for space vehicles Patent
Digital computer system for automatic prelaunch checkout of spacecraft
Johnson, H. G.↗
Acceptance checkout equipment for spacecraft
Design requirements and development of acceptance checkout equipment for spacecraft
Parsons, W. E.↗
Validation device for spacecraft checkout equipment Patent
Portable equipment for validating C band launch pad antennas and transmission lines used for spacecraft checkout
Cribb, H. E.↗
Space shuttle propulsion systems on-board checkout and monitoring system development study. Volume 1 - Summary Final report
Development of onboard checkout equipment and performance monitoring capability for space shuttles - Vol. 1
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Space shuttle propulsion systems on-board checkout and monitoring system development study. Volume 2 - Propulsion system definition and criteria Final report
Description of design reference model for space shuttle propulsion system onboard checkout and monitoring equipment to establish design criteria - Vol. 2
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Space shuttle propulsion systems on-board checkout and monitoring system development study. Volume 3 - OCMS criteria and concepts Final report
Criteria and concepts for onboard checkout and monitoring system for space shuttle propulsion system - Vol. 3
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Engine onboard checkout system study
Design and implementation of space shuttle propulsion system onboard checkout and monitoring function
Vandekoppel, R. W.↗
Space Shuttle Propulsion Systems On-board Checkout and Monitoring System Development Study. Volume 4: Appendices
Space shuttle propulsion systems onboard checkout and monitoring systems development study - appendices
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An engineering study of onboard checkout techniques. Task 1: Requirements analysis and concepts
Concepts and requirements analysis for automated onboard checkout of manned space station
Mckinley, A. P.↗
An engineering study of onboard checkout techniques. Task 2: Software
Language and executive software requirements for automated onboard checkout of manned space station
Welsh, D. M.↗
On-line software checkout facility for special purpose computers
On-line software checkout facility for special purpose computers used in developing spaceborne programs
Hughes, J. S.↗
The mobile concept and automated checkout of the Apollo/Saturn V space vehicle
Mobile concept and automated checkout applications in Apollo/Saturn 5 Launch Complex 39, discussing performance
Marshall, J. M.↗
Software control for large scale on-board checkout: A concept
Two level system checkout in which first level satisfies continuous monitoring requirements and second level provides fault isolation to satisfy maintenance requirements, provides self-checking capability for monitoring system and enables recovery from unexpected error or failure interruptions. System must perform operational duties of navigation, control, and experimentation.
Grounds, H. K.↗
A guide to onboard checkout. Volume 7: RF communications
The radio frequency communications subsystem for a space station is considered, with respect to onboard checkout requirements. The subsystem comprises all equipment necessary for transmitting and receiving, tracking and ranging, command, multiple voice and television information, and broadband experiment data. The communications subsystem provides a radio frequency interface between the space station and ground stations, either directly or indirectly, through a data relay satellite system, independent free-flying experiment modules, and logistics vehicles. Reliability, maintenance, and failure analyses are discussed, and computer programming techniques are presented.
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