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Results for “Comparative Study” 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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At least 685 records · Page 38NASA NTRS 1966
System and subsystem design concepts for Mars probe/lander entry from interplanetary approach trajectory or orbit mission modes
NASA NTRS 1966
Mars probe-lander capsule system and subsystem descriptions based on entry from approach trajectory
NASA NTRS 1966
Mission and system specifications for Mars probe based on capsule entry from interplanetary approach trajectory
NASA NTRS 1966
System design for nonsurvivable Mars probe deployed from orbiting spacecraft to perform engineering experiments for atmospheric and terrain property determination
NASA NTRS 1966
Mission system and subsystem specifications for Mars probe deployed from planetary vehicle orbiting around Mars
NASA NTRS 1966
Subsystem development status and ground development tests for Mars probe and recommended flight tests
NASA NTRS 1966
Sterilization considerations for Mars probe space vehicle - biological burden estimate, control, verification, and maintenance
NASA NTRS 1966
Trajectory analysis for Mars probe for entry from approach hyperbola or from Mars orbit
NASA NTRS 1966
Aerodynamics, thermodynamics, thermal control, and structural mechanics for Mars probe entry shell
NASA NTRS 1966
Telecommunication, electrical power and radar subsystem studies for Mars probe
NASA NTRS 1966
Mars probe instrumentation selection, systems interface, and payload definition
NASA NTRS 1966
Mars probe attitude control and propulsion system
NASA NTRS 1966
Mars probe flight capsule mechanical subsystems for trajectory and orbital entry
NASA NTRS 1966
Data correlations on forced-convective heat transfer to cryogenic fluids by nucleate, film and transition region boiling
NASA NTRS 1966
Electric power generator selection for Mars probe/lander
NASA NTRS 1965
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NASA NTRS 1966
Fatigue crack propagation in thin plates under fluctuating plane extension and cylindrical bending
NASA NTRS 1966
Size, type, and cost of facility simulating 200,000 ft altitude for testing small chemical rockets and components