Precision Landing Performance of a Human-Scale Lunar Lander Using a Generalized Simulation Framework
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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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The proposed concept is a redesign of the Tension Adjustable Network for Deploying Entry Membrane (TANDEM) tensegrity rover for a low-cost mission to Mars. Focus is on the entry, descent, landing, and locomotion (EDLL).
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Summary of Capabilities that can enable long-duration operations for missions on planets with extreme conditions like Venus and Mercury.
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Heating and cooling time calculation for planetary landing system survival payload
Engineering and conceptual design of landing system for Voyager unmanned spacecraft
Hourly precipitation data from four weather stations over a 13-year period presented in SIPLIC form with aid of IBM 1620 computer
Use of lift to increase payload of unmanned Martian landing capsule, discussing approach corridor and capsule design
Use of lift to increase payload of unmanned Martian landing capsule, discussing approach corridor and capsule design
Surveyor E instrumentation, propulsion and control systems, and flight plans
Sterilization environment effects on structural systems design for interplanetary spacecraft