Definition of entry corridor thermal limits for Apollo spacecraft.
Entry corridor thermal entry limits for Apollo spacecraft defined for design of thermal protection system
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Entry corridor thermal entry limits for Apollo spacecraft defined for design of thermal protection system
Photographic control system requirements for Project Apollo manned launches, considering extreme heat, vibration and sound pressure environment
Sensible heat exchange from Gemini and Apollo space suits determined in environmental test facilities, presenting data for heat flux distributions
Radiation protection plan for Apollo lunar mission based on real time monitoring of solar activity and radiation in spacecraft
Thermochemical and mechanical ablation mechanisms for Apollo heat shield material, comparing surface thermochemistry computer program and arc plasma tunnel data
Radiation measurements inside Apollo 4 and 6 command modules during passage through trapped radiation belts
Complex digital computers designed for Apollo spacecraft missions, discussing construction techniques
Clinical report on Apollo 7 and 8 mission medical data, discussing preflight preventive medical activities, inflight treatment, radiation levels, etc
Apollo LM and CSM tracking systems boresight shift reducible by decreasing modulation indices or scaling factor alpha
Apollo mission simulation, discussing Command Module Simulator /CMS/, onboard computer system and dynamic visual presentation via infinity- optics display
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Aerodynamic measurements on Apollo CM model at hypersonic flow simulating earth orbital reentry trajectory
Thermal vacuum /TV/ manned test operations related to Apollo lunar module in simulated space environment
Saturn 5 boost phase environment simulation on Apollo stages, discussing fixtures, load devices, instrumentation and ground test
Static structure ground test for Saturn-Apollo vehicle short stack, describing air pressure simulation, data acquisition and readout systems
Baker-Nunn photometry from Apollo tracking utilizing photographs for brightness, dynamics and duration of rocket exhausts and venting clouds
Apollo optics system ground and flight performance tests results, suggesting possible design changes for sunlit space environments
Heights of cloud bases and convective cloud tops determined by stereoscopic photogrammetry of Apollo 6 mission