An experimental checkout system was built for demonstrating a method of assisting the astronaut to cope with all his various data management requirements. Data from two functionally simulated, critical spacecraft subsystems and one experiment apparatus were sent through a model telemetry system to a computer having characteristics similar to those of available spacecraft computers. A wide variety of malfunction situations could be inserted into the subsystem hardware. Through software design, the major checkout functions of status monitoring, malfunction detection, and fault isolation were incorporated into a system which included a computer-drive n alphanumeric readout device. Astronaut control was provided through a display and keyboard unit installed in a space-station simulator that provided a "cockpit" environment. Stimulus generation was minimized in favor of fault isolation based on performance analysis of the equipment being tested. The experiment verified the design approach and provided a tool for evaluating man-machine interaction in subsequent revisions of the system. Background N UMEROUS reports have discussed the requirements for an onboard checkout system (OBCS) to be used on postApollo programs (1) and (2). The OBCS simulator project described in this paper was an independent development program performed in support of an Apollo Application Program (AAP) study contract. It was structured to be applicable to existing hardware. For the purposes of this discussion, an OBCS is defined as one capable of automatically monitoring and checking inflight spacecraft equipment. The Apollo spacecraft is sufficiently instrumented to permit isolation of malfunctionin g equipment by using the onboard telecommunications system, but such equipment would not be considered as an OBCS. Only onboard equipment that can automatically and rapidly provide status monitoring, malfunction detection, and malfunction isolation of all spacecraft systems would properly fit our description of an OBCS. Another aspect of OBCS which is beyond the more usual categories of spacecraft instrumentation is provision for onorbit maintenance and experiment readiness checks. This represents a capability not emphasized in present systems, but for which future requirements will exist. Planned mission objectives include the acquisition of large volumes of data from a wide variety of experiments to be conducted from an orbiting laboratory during manned missions extended to 120 days, with certain modules manned by different crews for up to 365 days. Under computer control, an OBCS would relieve the astronaut from performing tasks such as onboard data acquisition and processing, status monitoring, malfunction detection, and fault isolation involved in the operation and in in-flight maintenance of both experiment and spacecraft equipment.