Heat sterilization of pyrotechnics and onboard propulsion subsystems
Heat sterilization of pyrotechnics and spacecraft onboard liquid and solid propulsion subsystems
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Heat sterilization of pyrotechnics and spacecraft onboard liquid and solid propulsion subsystems
Onboard centrifuge as prophylactic and therapeutic device to prevent debilitation from effects of weightlessness during extended manned space missions
Principles of constructing diagnostic algorithms and programs for automatic medical monitoring and investigations by digital computers onboard manned spacecraft
Onboard checkout equipment design requirements, considering hardware and software for manned spacecraft flight
An overall plan for onboard rendezvous operations for the Gemini missions was developed in parallel with the mission plan. The purpose of this plan was to make optimum use of crew time in orbit to maximize the probability of a successful rendezvous. The evolution of the plan began with a preliminary time line of events based upon the known guidance-equipment requirements and upon the estimated crew timing. A preliminary set of flight charts was developed to aid the crew with primary and backup procedures and to establish a backup guidance capability. These charts, which consisted of a few simple graphs and tabulation sheets, enabled the crew to calculate accurate solutions for the terminal maneuvers even with an inoperative guidance-equipment component. As such, the charts significantly contributed to the probability of mission success. Following the development of the charts, an engineering evaluation was conducted on a realistic man-in-the-loop simulation. During this evaluation, the procedures and charts were subjected to the expected equipment errors and trajectory dispersions, and revisions were made as necessary to improve effectiveness. The resulting plan was presented to the flight crew; the charts were evaluated during a period of training on the simulator. The crew spent several weeks training on both the primary procedures and on the various failure modes.
Performance/design criteria for aid in selecting onboard checkout and data management system computers
Onboard checkout and data management system
Specifications for computer program support system for onboard checkout and data management system
System logic, data acquisition process, and digital data transmission system of onboard checkout and data management system
Supervisory computer program for onboard checkout and data management system of Saturn/Apollo application program
Spacecraft attitude determination using single onboard camera
Automatic closed loop onboard nutation control system for unstable asymmetrical spin stabilized spacecraft, analyzing Applications Technology Satellite system and performance
Performance and design criteria for onboard checkout data management system control and display units, and man machine interfaces
Design and operation of onboard spacecraft computer
Temperature control of transparent elements onboard artificial satellites
Optimal shielding criteria for nuclear apparatus onboard spacecraft
Computer onboard checkout for space stations of mid- 1970
Ground based guidance systems for supplementing onboard guidance of manned space vehicles