Heat-shield ablation measurements using radioisotope techniques
Radioactive isotope technique for heat shield ablation measurement during reentry
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Radioactive isotope technique for heat shield ablation measurement during reentry
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angles of attack
Newtonian flow model for aerodynamic analysis of reentry vehicle body geometry
Expansion tube for simulating hypervelocity flow conditions for reentry vehicles
Oxidation and ablation behavior during simulated reentry of metals and alloys for use in NERVA REACTOR
Langmuir probes for determining electron density surrounding reentry vehicles
Simulation study of manual control capability for Apollo spacecraft reentry orientation after high altitude launch abort using visual scene
Planned astronaut training, preflight operations, flight activities, and reentry for Gemini 9
Progress and problems in atmospheric entry for manned and unmanned planetary probes - reentry physics
Electron attachment to atomic fluorine in thermally ionized air for application to reentry radio communications blackout
High temperature, oxide-dispersion hardened alloy uses in turbojet engines, reentry vehicles, and other applications
Wide beam radio interferometer system for reentry tracking of Apollo spacecraft
Interfacial stability of two parallel superposed inviscid streams of fluid applied to stability of molten liquid-gas interface on ablating reentry body
Heat shielding and material testing for manned Mars landing and hyperbolic reentry missions
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle heat shields
Aerodynamic characteristics of pyramidal reentry shapes with variable geometry, at subsonic speeds
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
Airborne infrared detection, acquisition, and tracking system for Apollo command module reentry