Browse Items (6 total) Browse All Browse by Tag Search Items Subject is exactly "Data processing" Sort by: TitleCreatorIdentifierDate Added "Automatic Pressure Transducer Calibration System." Schuler, Albert E. 1967-11-29 "Automated PCM Data Processor Theory of Operation." Toney, J. 1966-01-01 "Technical problems in on-board checkout systems." Smith, Robert L. 1968-01-01 "Spacecraft television ground data handling system." General Precision, Inc. Link Division 1967-01-01 "Interface Control Document Definition of Saturn SA-507 Flight Sequence Program." George C. Marshall Space Flight Center. Airborne Electrical Systems Branch 1967-12-05 "Computer Controlled Power Application for the Saturn Launch Vehicle". Felber, Henry D. 1967-08-01 Output Formats atom, csv, dc-rdf, dcmes-xml, json, omeka-xml, rss2 Refine search Identifier Select...Compcontpowe.pdfInterControlDocu.pdf TWO COPIESSpactelegroudata_022508152653.pdfspc_stnv_000133spc_stnv_000135spc_stnv_000205spc_stnv_000344spc_stnv_000839spc_stnv_000873TechProbOnBo_062408092345.pdf Title Select..."Automated PCM Data Processor Theory of Operation.""Automatic Pressure Transducer Calibration System.""Computer Controlled Power Application for the Saturn Launch Vehicle"."Interface Control Document Definition of Saturn SA-507 Flight Sequence Program.""Spacecraft television ground data handling system.""Technical problems in on-board checkout systems." Alternative Title Select...0M33627BIBM No. 67-U60-0019NASA TM X-53678 Description Select...A design report which displays and explains how the Spacecraft Television Ground Handling System functions, is designed and what it might be used for in the future.For the purposes of this paper, an onboard checkout system is defined as a system which is built into prime flight equipment, flies with it, and permits a checkout capability to exist during all the major phases of the test and mission life of that prime equipment. Varying degrees of capability may exist in such a system, depending on what is designed into it. This, in turn, is generally dependant on life and mission requirements of the prime equipment, degree of mission checkout required, reliability restrictions,redundancy levels, data management scheme, and equally important, state of the art . Not all checkout can be accomplished with onboard equipment. Mechanical system problems such as leak detection, for example, require techniques that cannot be remotely controlled and evaluated today. On the other hand, such things as in-flight telemetry have been used for quite a long time and will continue to be used for onboard checkout.Includes a blueprint of DDAS System Block Diagram.The abstract notes, "The development of an automatic pressure transducer calibration system is discussed in this report. Evolution from past practices and systems into an automatic calibration system with computerized data handling is described."The purpose of this document is to define the flight sequence events, time bases, stage switch selector channel assignments, LVDA Discrete Outputs, Inputs and Interrupts for the Saturn SA-507 & Subs vehicles. Special requirements and restrictions defined in this document will be imposed on the Marshall Space Flight Center and its contractors as applicable, to insure the proper functioning of the equipment in the various stages for required vehicle timing and sequencing to occur as outlined in this Interface Control Document (ICD).This paper describes a real-time digital computer program that controls the application of electrical power to the S-IVB stage of the Saturn vehicle at Cape Kennedy, Florida. Douglas Aircraft Company, the S-IVB stage manufacturer, provided NASA with the program requirements relative to the energizing sequence, voltage and current measurement tolerances, and vehicle system operational tests. International Business Machines Corporation provided NASA with the computer program to satisfy the task requirements. The program conjoined the components of the Electrical Support Equipment (two RCA 110A computers and control and instrumentation devices) into a closed loop system. The supporting operating system program by IBM is described. Creator Select...Felber, Henry D.General Precision, Inc. Link DivisionGeorge C. Marshall Space Flight CenterGeorge C. Marshall Space Flight Center. Airborne Electrical Systems BranchSchuler, Albert E.Smith, Robert L.Toney, J. Temporal Coverage Select...1960-1969 Subject Remove filter...Data processing Type Select...Design ReportsEssaysProposalsReportsTechnical reportsText Language Select...en
