Ground installations for development, qualification, and checkout testing of the apollo space vehicle.
Ground installations for development, qualification and checkout testing of Apollo space vehicle
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Ground installations for development, qualification and checkout testing of Apollo space vehicle
Checkout equipment built as integral part of space vehicle stage
Acceptance checkout equipment and spacecraft testing
Facility for sterilization of space flight vehicles permitting sterile access to flight hardware for assembly, checkout and repair
Checkout criteria and requirements for manned spacecraft, specifically Apollo
Hardware, software, and evaluation of digital computer systems used in various phases of automatic space vehicle checkout
Space vehicle stage checkout in Saturn launch application
Computer applications in checkout of individual Saturn stages and in prelaunch checkout of complete Saturn vehicle
Electronic checkout, environmental qualification and integration of OGO by spacecraft simulator and performance analysis system
Ground installations for development, qualification and checkout testing of Apollo space vehicle
Space vehicle checkout procedure application to near-future transport aircraft, noting NASA SPONSORED advances
Improvements in space vehicle stage checkout, structural nondestructive testing, and electronic component testing within quality control program
Apollo/Saturn V automatic checkout test verification and debug program using real time computer simulation with digital space vehicle system model
The Launch Processing System represents Kennedy Space Center's role in providing a major integrated hardware and software system for the test, checkout and launch of a new space vehicle. Past programs considered the active flight vehicle to ground interfaces as part of the flight systems and therefore the related ground system was provided by the Development Center. The major steps taken to transform the Launch Processing System from a concept to reality with the successful launches of the Shuttle Programs Space Transportation System are addressed.
The GOAL (Ground Operations Aerospace Language) test programming language was developed for use in ground checkout operations in a space vehicle launch environment. To insure compatibility with a maximum number of applications, a systematic and error-free method of referencing command/response (analog and digital) hardware measurements is a principle feature of the language. Central to the concept of requiring the test language to be independent of launch complex equipment and terminology is that of addressing measurements via symbolic names that have meaning directly in the hardware units being tested. To form the link from test program through test system interfaces to the units being tested the concept of a data bank has been introduced. The data bank is actually a large cross-reference table that provides pertinent hardware data such as interface unit addresses, data bus routings, or any other system values required to locate and access measurements.
GOAL, is a test engineer oriented language designed to be used to standardize procedure terminology and as the test programming language to be used for ground checkout operations in a space vehicle launch environment. The material presented concerning GOAL includes: (1) a historical review, (2) development objectives and requirements, (3) language scope and format, and (4) language capabilities.
Launch automation programs for Saturn IB SYSTEM utilizing digital computer techniques to increase vehicle reliability from manufacturing through prelaunch checkout
Results of a life science impact analysis for accommodation to the Space Station of a manned Mars mission are discussed. In addition to addressing such issues as on-orbit vehicle assembly and checkout, the study also assessed the impact of a life science research program on the station. A better understanding of the effects on the crew of long duration exposure to the hostile space environment and to develop controls for adverse effects was the objective. Elements and products of the life science accommodation include: the identification of critical research areas; the outline of a research program consistent with the mission timeframe; the quantification of resource requirements; the allocation of functions to station facilities; and a determination of the impact on the Space Station program and of the baseline configuration. Results indicate the need at the Space Station for two dedicated life science lab modules; a pocket lab to support a 4-meter centrifuge; a quarantine module for the Mars Sample Return Mission; 3.9 man-years of average crew time; and 20 kilowatts of electrical power.