Development and Operation of a High Altitude Balloon Payload (Rev. 1) [Slides]
Project Goals: Develop a high-altitude balloon payload that can communicate live data up to 50000 meters; Collect and analyze neutron data.
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Project Goals: Develop a high-altitude balloon payload that can communicate live data up to 50000 meters; Collect and analyze neutron data.
ARM Aerial Facility (AAF) Portable Optical Particle Counter (inside payload bay)
ARM Aerial Facility (AAF) Portable Optical Particle Counter (inside payload bay)
Payload designed to measure the electron density of the ionosphere
Optimization of propulsion system and trajectory parameters of a power-limited space vehicle to achieve maximum payload with application to earth-mars rendezvous missions
Pressure measurement at instrument rack of sounding rocket payload after nose cone ejection
Nike-Apache rocket payloads for upper atmosphere ionization measurement and wind determination
Magnetic decontamination program for Pioneer satellite and scientific payload
Computer program for Project Fire 1 payload reentry flight angle of attack analysis
Effect of hydrogen snow accumulation on Centaur retromaneuver and Surveyor payload
Photometric analysis of spectrograms of two Trailblazer I payload reentry events
Payload weight and length effect on mass and aerodynamic characteristics of Apache and Cajun sounding rockets
Computer program for evaluating space experiments for Saturn in-flight payloads - experiment design
Terminal shock-boundary layer interaction on slender cone-cylinder payloads at supersonic speeds and resulting flow separation
Sterilizability of scientific payloads for planetary exploration
Balloon payload orientation system for viewing fixed position on celestial sphere
Terminal shock-boundary layer interaction on slender cone-cylinder payloads at supersonic speeds and resulting flow separation
Optimal payload trajectory characteristics for winged booster vehicles