Emc control effort on the ace-s/c system /apollo program/
Electromagnetic interference control effort for ground support system which automatically checks systems in command service and LEM for Apollo program
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Electromagnetic interference control effort for ground support system which automatically checks systems in command service and LEM for Apollo program
Structural and systems design of Apollo lunar excursion module in terms of operational requirements
Structural features of Apollo spacecraft, its subsystems, configurations and functions
Guidance and navigation equipment used by both Apollo service module and lunar excursion module
Technical development status of project Apollo lunar excursion module
Earth and lunar trajectory and landing site requirements for lunar excursion system
LEM docking with command module in lunar orbit, noting need for visual aids for alignment information
Solid state radar transmitter design for lunar missions noting velocity sensor and altimeter functions, packaging details, thermal problems, etc
Surveyor Lunar Roving Vehicle /SLRV/ mission in support of Apollo LEM program
Solid-liquid systems sized for 1971 and 1973 missions and 1975 and 1977 missions, Apollo lunar excursion module descent propulsion system, and Titan III-C transtage
Some 22 years have elapsed since the first digital computer was completed. For the past several years, digital guidance computers have flown in airplanes, missiles, and rockets. Some of these vehicles are scarcely bigger than an early computer, whose performance is surpassed by the guidance computers they carry.
Apollo mission and spacecraft, astronaut clothing and training, and experiments necessary for manned lunar exploration - conference.
Command, service, and excursion modules of lunar exploration spacecraft, and communication links with earth stations
Systems design study for earth visible and astronaut visible lunar solar reflecting beacons to aid in descent and landing of lunar excursion module and other lunar landing vehicles
Stress and deformation analysis for Apollo lunar excursion module adapter under mechanical and thermal loading
Navigation, guidance and control systems to meet basic trajectory and crew safety requirements of LEM
Measurement schedules effect on work load of astronaut performing navigation function, stressing tradeoff between number of measurements and accuracy level