Study of plasma sheath associated with communications blackout Final report, Jun. 1963 - Dec. 1966
Bibliography of technical reports on plasma sheath phenomena and communications blackout during vehicle atmospheric reentry
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Bibliography of technical reports on plasma sheath phenomena and communications blackout during vehicle atmospheric reentry
Effects of atmospheric reentry on graphite particles
Recovery of reentry rocket by sound ranging detection of shock wave
Symmetrical equilibrium flow past blunt body at superorbital reentry conditions calculated by integrating motion equations across shock layer
Gemini spacecraft antennas performance during reentry into ionized medium, discussing electron concentration profiles, nonearth atmosphere extrapolation and antenna breakdown effect
Raytheon 440 computer for simulation of spacecraft reentry simulation
Error analysis of hybrid simulation for six degree of freedom equations of motion for spacecraft reentry
Handling qualities, disturbances and reentry corridor boundaries for spacecraft control system design
Computer program for simulating single-pass and single-skipout trajectories for lifting reentry vehicles
Quasilinearization method applied to optimal control problem computations - reentry trajectories
Catalytic efficiency calculations for surface heat flux and heat transfer during atmospheric reentry
A parametric analysis of a radioisotope-thermoelectric power generator is presented. A cylindrical heat-source geometry was assumed with either lead telluride or silicon-germanium thermoelectric elements located around the lateral surface of the fuel block. Generator performance, rather than overall power-system performance, was analyzed; that is, such mission dependent considerations as nuclear shielding, reentry protection, and power conditioning were not included.
Modified control logic with random-number procedure to determine error effects on range controller of reentry vehicle
The Gemini Program was conceived to provide a space system that could furnish answers to many of the problems in operating manned vehicles in space. It was designed to build upon the experience gained from Project Mercury, and to extend and expand this fund of experience in support of the manned lunar landing program and other future manned space-flight programs. The purpose of this paper is to relate some of the results of the Gemini Program to the Apollo Program, and to discuss some of the contributions which have been made. The objectives of the Gemini Program applicable to Apollo are : (1) long-duration flight, (2) rendezvous and docking, (3) post-docking maneuver capability, (4) controlled reentry and landing, (5) flight- and groundcrew proficiency, and (6) extra vehicular capability. The achievement of these objectives has provided operational experience and confirmed much of the technology which will be utilized in future manned programs. These contributions will be discussed in three major areas : launch and flight operations, flight-crew operations and training, and technological development of subsystems and components. While there is obvious interrelation among the three elements, the grouping affords emphasis and order to the discussion.
FORTRAN computer program for calculating model planetary atmospheres and density and temperature dispersion data for Apollo reentry
Complex metal oxides, reentry temperature systems, and elastic wave propagation through rocks at elevated temperature and pressure
Spectrometric techniques for estimating flow field gas temperatures of reentry vehicles
Vibrational relaxation in supersonic nozzle diatomic gas flow, nonequilibrium effects in high enthalpy airflow over thick wedge flat plates, and reentry nonequilibrium flow fields