Spacecraft launch preparation
Ground checkout and prelaunch testing of Gemini spacecraft - launch site operations
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Ground checkout and prelaunch testing of Gemini spacecraft - launch site operations
A tri-axis flux-gate magnetometer was used on four Gemini spacecraft for determination of the magnitude and direction of the local geomagnetic field with respect to the spacecraft. Conclusions derived from the data are not only important to the proton-electron spectrometer experiment, but also are of significance to any directional charged particle experiments that may be conducted. Even though the Gemini spacecraft was not clean magnetically, the data could be reduced to a form that supplied directional information on the magnetic field in relation to the spacecraft. Stray fields were the result of spacecraft structure, not the result of current flows that were produced within the spacecraft electrical systems. Efforts were made to reduce spacecraft stray fields and to facilitate the acquisition of more accurate data.
Dim light photography and visual observations of space phenomena from Gemini spacecraft
Modular concept of operations, manufacturing working plan, management communications, and procedures control for development of Gemini spacecraft
Micrometeoroid impact experiments conducted on Gemini 9 and 12 missions
Flight sequence, capsule design, pyrotechnic applications, escape modes, and safety features for Gemini spacecraft
Gemini spacecraft reliability and quality control test program
Power sources for Gemini spacecraft electrical systems, load sharing of fuel cells during flight, and sequential system for electrical control of spacecraft
Communications and instrumentation systems for Gemini spacecraft - pulse code modulation equipment on Gemini II through VII
Nuclear emulsion measurements on particle populations in space using sounding rockets and Gemini spacecraft
Simulation testing pilot performance in orbiting Gemini spacecraft based on tracking rate errors and fuel consumption
Celestial navigation design for enabling astronaut to determine location of orbiting Gemini spacecraft by visual comparison of actual star field to representation on device
Astronaut performance and response during Gemini spacecraft flights
Effects of edge constraints on optical qualities of Gemini spacecraft windows
Project Gemini - spacecraft, space suits, astronaut selection and training, Gemini-Titan and Atlas-Agena launch vehicles, Gemini missions, and brief outline of Project Apollo
Translational Cell and Animal Research (TCAR). For nearly 50 years, the NASA Space Biology Program has funded, and Ames Research Center (ARC) has managed, a robust program of fundamental research including studies using a wide range of animal cells, tissues and organisms. Much of this research was conducted on spacecraft in microgravity environments including diverse platforms such as: Gemini Spacecraft, US Biosatellites, Apollo Command Modules, Skylabs, Russian Biosatellites, NASA Space Shuttles, NASA/Mir, and most recently, the International Space Station (ISS). During the Space Shuttle Era (1981–2011), the science of space biology took an enormous step forward with 45 missions that afforded researchers with new opportunities to conduct systematic and complex experiments aimed at a deeper understanding of how life adapts to the space environment. Beginning in the 1990s, the products of these experiments, comprised of research summaries and rare, unused biospecimens, were collected and catalogued within the ARC Life Sciences Data Archiving Office, a branch of NASA’s Life Sciences Data Archive (LSDA) managed from the NASA Johnson Spaceflight Center.
Space shuttle electronics requirements, considering systems in Mercury and Gemini spacecraft and Apollo lunar and command service modules
Analytical method for determination of window induced navigation instrument errors in Gemini spacecraft