Reentry communication by material addition Patent
Reentry communication by injection of water droplets into plasma layer surrounding space vehicle
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Reentry communication by injection of water droplets into plasma layer surrounding space vehicle
Properties of fluids around blunt reentry bodies and application to reentry communications blackout problem
Evaluation of material additive technique used on Gemini III mission for alleviation of communications blackout
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X-band telemetering for radio interference - reentry communication in earth orbit reentry vehicle
Gemini mission experimental results on zodiacal light photography, radiation effects on blood, cloud-top spectrometry, star occultation navigation, and reentry communications
Plasma sheath effect on reentry communication system with slot antennas
Antenna radiation patterns and near field effects by solving aperture and plasma sheath problems independently in reentry communications
Measurement of thermal accommodation coefficients between liquids and high temperature gases in low pressure reentry communications blackout intervals
The objective of this flight demonstration is to deploy a slender-body hypervelocity aerodynamic research probe (SHARP) from an orbiting platform using a tether, deorbit and fly it along its aerothermal performance constraint, and recover it intact in mid-air. To accomplish this objective, two flight demonstrations are proposed. The first flight uses a blunt-body, tethered reentry experiment vehicle (TREV) to prove out tethered deployment technology for accurate entries, a complete SHARP electronics suite, and a new soft mid-air helicopter recovery technique. The second flight takes advantage of this launch and recovery capability to demonstrate revolutionary sharp body concepts for hypervelocity vehicles, enabled by new Ultra-High Temperature Ceramics (UHTCs) recently developed by Ames Research Center. Successful demonstration of sharp body hypersonic vehicle technologies could have radical impact on space flight capabilities, including: enabling global reentry cross range capability from Station, eliminating reentry communications blackout, and allowing new highly efficient launch systems incorporating air breathing propulsion and zeroth staging.
Description of an x-band telemetry receiving system for communication during reentry
Electron attachment to atomic fluorine in thermally ionized air for application to reentry radio communications blackout