Study of expandable, terminal decelerators for Mars atmosphere entry Interim summary report, Dec. 1965 - Jun. 1966
Design of expandable terminal decelerators for Mars atmosphere entry by Mars-lander capsule
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Design of expandable terminal decelerators for Mars atmosphere entry by Mars-lander capsule
Spacecraft control studies on antenna pointing, capsule sterilization, propulsive lander, optical sensing for soft landing spacecraft, and gyro data reduction computer programs
Approximate methods in electric propulsion missions such as lunar orbiter lander
Communication parameters associated with Martian flyby probes and with lander and manned vehicles
System design of Voyager-class Mars Probe/ Lander, considering selections of entry aeroshell, landed capsule and descent and postimpact instrumentation
Mars landing guidance requirements for unmanned lander after separation from interplanetary flyby space vehicle
Thermophysical research requirements for Venus Lander, Jupiter Entry Probe and Mercury Orbiter planetary exploration missions
Techniques for sterilization of planetary probes and landers to prevent contamination of exobiological instrumentation, tests, and planetary biospheres
Advanced multiprocessor computer organization for manned Mars lander mission
Transtage and piggyback payloads, planetary entry parachute, Voyager lander, lifting body and Apollo applications programs at Martin Marietta
Lunar photographic methods and data including flyby, impacter, lander and orbiter photographic missions
Mission and planetary vehicles characteristics affecting design of solid propellant motors and thrust vector control systems in planetary orbiters and landers
Asteroid mission objectives and requirements, discussing asteroid lander and flyby missions
Soft lander support module for Mars missions - summary
Soft lander support module for Mars missions - subsystem studies
Soft lander support module for Mars missions - lunar module radar evaluation and vernier phase simulation
Environmental analysis of planet Mars, computer program, design of Martian hard-lander solar array, and shock tests
Pyrolysis, hydrogen flame detectors and gas support systems for use in life detection system on Mars lander mission