MARINER VENUS '62 FLIGHT TELECOMMUNICATION SYSTEM
Mariner /venus 62/ flight telecommunication system for data transmission and trajectory determination
DATA TRANSMISSION↗
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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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SYSTEM CHECKOUT AND FLIGHT TESTING OF UNMANNED LUNAR AND PLANETARY SPACECRAFT
Test equipment, facilities and types of tests involved in system checkout of the ranger and mariner spacecrafts
SYSTEMS ANALYSIS↗
Mariner Mars 1964 Missions Scheduled for Early November
Mission plans for mariner mars 1964
MARS /PLANET/↗
Mariner mars 1964 telemetry and command system
Telemetry and command system for Mariner-Mars 1964 mission
TELEMETRY↗
Mariner 1964 probability of success model
Mathematical model of Mariner mission success probability
SPACECRAFT RELIABILITY↗
Heat-sterilizable power source study for advanced Mariner missions
Heat sterilizable power sources for Mariner Mars landing capsule
MARINER PROGRAM↗
A redundant spacecraft sequencer breadboard Phase I report, Dec. 22, 1965 - Mar. 30, 1966
Combined integrated and discrete circuit breadboard model for redundant multiple logic version of Mariner C spacecraft central computer and sequencer
REDUNDANT SYSTEM↗
Scientific results of Mariner missions to Mars and Venus
Scientific results of Mariner II and Mariner IV missions to Mars and Venus, measurements of exospheric structure, and spacecraft systems designs and trajectories
VENUS PROBE↗
Science payloads from Mariner II to Mariner IV
Scientific instrumentation design for 1962 and 1964 Mariner spacecrafts
INSTRUMENTATION↗
Mariner Mars 1964 acoustically induced vibration environment
Estimation of lift-off and transonic vibration spectra on Mariner Mars 1964 spacecraft to enhance survival probability in acoustically induced vibration environment during boost phase
VIBRATIONAL SPECTRUM↗
Mariner Mars 1964 project report - Mission and spacecraft development. Volume II - Appendixes
Mission planning and spacecraft development for Mariner Mars project
MISSION PLANNING↗
Venus DSS operations
Venus Deep Space Station experiments involving telemetry with Mariner IV spacecraft in cooperation with Mars Deep Space Station
TELEMETRY↗
Review of Mariner 1962 and 1964 spacecraft design and operational planning.
Unmanned interplanetary long-duration Mariner space flights and instrumentation, guidance, control, stabilization and communications of Mariner II and IV
MARINER IV SPACE PROBE↗
Ranger and Mariner temperature control experiences.
Ranger and Mariner spacecraft temperature control design, test and flight results
MARINER PROGRAM↗
The evolution of the Mariner spacecraft.
Mariner space vehicles design evolution noting contribution to future space flights through measurement of atmospheric density of Mars
SPACECRAFT DESIGN↗
A structural view of solar array developments.
Spacecraft structural criteria for lightweight photovoltaic solar arrays development, discussing Mariner type panel designs and power-to-weight ratios
SPACECRAFT STRUCTURE↗
A closed-loop automatic control system for high-intensity acoustic test systems.
Sound at sound pressure levels in the range from 130 to 160 dB is used in the investigation. Random noise is passed through a series of parallel filters, generally 1/3-octave wide. A basic automatic system is investigated because of preadjustment inaccuracies and high costs found in a study of a typical manually controlled acoustic testing system. The unit described has been successfully used in automatic acoustic tests in connection with the spacecraft tests for the Mariner 1971 program.
Slusser, R. A.↗