Telemetry test system
Telemetry system for rapid checkout for space tracking and data acquisition network
TRACKING↗
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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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The saturn v launch vehicle.
Design approach, testing and checkout program of Saturn V launch vehicle
LAUNCH VEHICLE↗
Saturn V Launch Vehicle Digital Computer and Data Adapter
Saturn V launch vehicle digital computer and data adapter for checkout and guidance functions
DATA CONVERTER↗
Solid state thermostat has integral probe and circuitry
Compact, reliable thermostat provides a temperature readout signal and a continuous temperature-control output for temperature monitoring by automatic checkout equipment or telemetry systems. It employs a solid state circuit in a housing rigidly attached to a thermistor probe.
Source record↗
Device serves as hinge and electrical connector for circuit boards
Hinge makes both sides of electrical circuit boards readily accessible for component checkout and servicing. The hinge permits mounting of two circuit boards and incorporates connectors to maintain continuous electrical contact between the components on both boards.
Bethel, P. G.↗
System monitors discrete computer inputs
Computer system monitors inputs from checkout devices. The comparing, addressing, and controlling functions are performed in the I/O unit. This leaves the computer main frame free to handle memory, access priority, and interrupt instructions.
Burns, J. J.↗
Ground support equipment
Telemetry and command checkout equipment, environmental simulation facilities, and ground support handling fixtures for Relay I satellite
RELAY I SATELLITE↗
Surveyor project status report, 27 November, 1964
Checkout of T-21 spacecraft, and television telecommunication tests - Surveyor project
TELECOMMUNICATION↗
Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA Run 1
Nuclear reactor simulator test - liquid hydrogen run, instrumentation and data acquisition system operational procedure checkout
LIQUID HYDROGEN↗
Space flight operations
Space flight operations - launch site, deep space instrumentation facility, operations complex, launch site, communications facility, and checkout facility
SPACE FLIGHT↗
Saturn antenna systems, SA-5, Volume 3
Saturn I /SA-5/ antenna system - checkout procedures for altimeter antenna, Azusa antenna radar antenna, and Mistram antenna system
SATURN I /SA-5/ LAUNCH VEHICLE↗
Orbital tube flare for tubing connectors
Marshall engineering personnel have developed and are now refining a new and unique method of mechanically flaring tubing. The system eliminates the use of the conventional split backing die which is used with most tube-flaring equipment. The Marshall-developed tool is adapted for use on standard Leonard 3-CP-HD flaring machines. The stationary split backing die is replaced in function with a die ring, whose i.d.-surface rolls or orbits around the o.d. of the tube flare zone. An i.d.-flaring cone moves axially and forces the metal against the rolling die to form the flare. Major advantages of this system are the elimination of flash, or split die marks, on the back angle of the flare, and improved flare-surface finishes, permitting more uniform sealing characteristics and improvements of the total geometric configuration of the flare as required by the MSFC specification MC-146. The Orbital Adapter system of tooling is currently being used to manufacture flared tube hardware for the Saturn V S-IO space launch vehicle at MSFC, for the Agena space launch vehicle (used for the Gemini project) at Lockheed, Sunnyvale, for LEM checkout equipment for Grumman, and for the Saturn S-IV-B space launch vehicle by Douglas Aircraft Company. Several other aerospace firms are evaluating the system for possible incorporation on their tube flaring requirements. Marshall engineers are now concentrating their efforts on refining and reducing the total cost of the overall system.
Tubing↗
Digital events evaluator
Real time digital event evaluator description for Saturn launch vehicle checkout
SATURN LAUNCH VEHICLE↗
Measurement of neutron spectra in liquid hydrogen Quarterly progress report, period ending Dec. 17, 1965
Neutron spectra measurement in liquid hydrogen, water cooled fast neutron source, thermal neutron measurements, and liquid hydrogen facility checkout using nitrogen
WATER↗
Information transfer systems in space communications
Space communication information transfer systems parameters for checkout engineers
INFORMATION↗
Timing of check out before a critical event.
Timing of checkout in system with constant failure rate
TIME FACTOR↗
Program computes single-point failures in critical system designs
Computer program analyzes the designs of critical systems that will either prove the design is free of single-point failures or detect each member of the population of single-point failures inherent in a system design. This program should find application in the checkout of redundant circuits and digital systems.
Brown, W. R.↗
Phase plane displays detect incipient failure in servo system testing
Computer based data conditioning and display technique detects incipient failure in servo system testing, for use in prelaunch checkout of complex nonlinear servomechanisms. These phase plane displays enable identification of, on line, unusual or abnormal servo responses which can be displayed compactly in the time domain on a cathode ray tube.
Affenito, F. J.↗