Estimates of nonequilibrium ionization phenomena in the inviscid Apollo plasma sheath
Nonequilibrium ionization in asymmetric plasma sheath determined for Apollo spacecraft at superorbital velocity reentry
REENTRY COMMUNICATION↗
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Results for “Reentry”
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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Noncontaminating separation systems for spacecraft /Project ZIP/
Noncontaminating systems for separating shroud and reentry body, second stage, or spacecraft from booster
REENTRY BODY↗
Apollo infrared acquisition and tracking system
Airborne infrared acquisition and tracking system for Apollo reentry vehicle
INFRARED DETECTOR↗
A supercircular entry guidance concept designed for maximum monitoring capability
Reentry vehicle guidance system for automatic or manual range control and with pilot monitoring capability
GUIDANCE SYSTEM↗
Theoretical and Experimental Investigations of Spacecraft Antenna Problems in the Varied Operational Environments of Far-out-space and Atmospheric Re-entry Semiannual Report, 1 Jan. - 31 Jul. 1966
Spacecraft antenna, aperture, and reentry problems
ANTENNA↗
Development of sensors to obtain in-flight ablation measurements of thermal-protection materials
Design and development of sensors for measuring ablative changes in space vehicle heat shield during reentry phase
ABLATION↗
Thermochemical ablation.
Thermochemical interaction between ablation material and environment during manned reentry, using mainly graphite and composite materials
REENTRY EFFECT↗
Experimental investigation of a charring ablative material exposed to combined convective and radiative heating.
Charring ablative materials effectiveness in combined convective and radiative heating as reentry shield
MATERIAL TESTING↗
High-resolution experimental spectra and theoretical studies of equilibrium radiation from a blunt body traveling at 37,000 ft/sec.
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
HIGH TEMPERATURE AIR↗
Re-evaluation of heat-transfer data obtained in flight tests of heat-sink shielded re-entry vehicles.
Stagnation point velocity and pressure distribution over heat-sink shielded reentry vehicle to test boundary layer heat transfer theories
HEAT SHIELD↗
The experimental performance of an arc-driven vortex type heater-accelerator.
Arc-driven vortex type heater-accelerator for possible use in reentry flight simulation
VORTEX GENERATOR↗
Atmospheric entry dynamics of small particles.
Terminal reentry and dynamics evaluation computer program for small particles, using point-mass calculation during initial phase and determining drag coefficient
FREE MOLECULAR FLOW↗
An alternate analysis of momentum deposition in the wake of a re-entry vehicle.
Momentum deposition in wake of reentry vehicle, discussing behavior of complex materials characterized by heat of ablation
MOMENTUM STORAGE↗
A wind tunnel free flight testing technique for nonplanar motion of spinning models.
Wind tunnel free-flight testing of reentry vehicle dynamics, noting capability for simultaneous two- dimensional viewing of model trajectories
TRAJECTORY ANALYSIS↗
Including re-entry heating in rocket engine thermal analyses.
Reentry heat flux condition transformation into specified convective coefficients and temperatures, accounting for variation of flux with wall temperature
REENTRY CONDITION↗
The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90
Aerodynamic characteristics of blunt, lifting body reentry configuration
AERODYNAMIC CHARACTERISTICS↗
Hollow cathode plasma penetration study Final report
Hollow cathode electron beam discharge for penetrating plasma sheath around reentry vehicle
PLASMA SHEATH↗
A Method for Determining Optimum Re-entry Trajectories
Determining optimum atmospheric reentry trajectories using Pontryagin maximum principle
PONTRYAGIN PRINCIPLE↗