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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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Aerodynamic and flight characteristics of variable geometry entry spacecraft during subsonic wing deployment and landing
Mars autonomous entry navigation, discussing flight path angle control with onboard sensors using realistic sun, Canopus and planet line of sight tracker accuracies
Thermal control of Mars entry capsule with fiberglass honeycomb sandwich shell analyzed with and without aft thermal curtain, emphasizing cruise-flight phase
NASA planetary entry parachute program for rocket launched and balloon deployment tests
Aerodynamic performance tests of autorotative unpowered rotor entry vehicle model at various Mach numbers and angles of attack
Adaptive control for Mars entry based on sensitivity analysis
Atmospheric entry-capsule dynamics, considering angle of attack motion under gravity forces influence and aerodynamic normal force stability relations
Mars entry capsule ionized wake producing circularly polarized antenna radiation null region, noting effect on communication blackout time
Vector matrix second order sensitivity equation application to Mars entry guidance, performing numerical simulation of second order sensitivity guidance and tabulating results
Transport properties calculated by Chapman-Enskog theory for high temperature-gas mixtures in planetary entry applications
Equations of motion for dynamic stability of rotor entry vehicles
Mach number and oscillation amplitude effects on transonic dynamic stability of half-angle cone planetary entry shapes
Aerodynamics of Mars entry probe lander configurations at Mach 10
Predicted communication boundaries for earth atmosphere entry of Apollo vehicle based on plasma density and electrical properties
Investigation of S band signal transmission through Apollo earth entry plasma
Design of facility for simulating Mars space capsule entry
Test facility for simulating thermodynamic environments of planetary atmospheric entry
Jet plume induced, flow separation on lifting entry model flat bottom by pressure distribution analysis