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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Gemini VII star sightings analyzed, using handheld space sextant in Gemini VI, discussing effect of bias, timing, angle measurement and trajectory errors
Pressure and altitude data for GT-2 flight test
Gemini IX experiment to photograph airglow, zodiacal light, and Milky Way
Gemini IX airglow horizon photography experiment
Gemini IX experiment to determine flux and thin film penetration characteristics of micrometeorites, lethal space effects on microorganisms, and probability of life in space
Data processing equipment and procedures for real time programming system used with Gemini manned missions
Network performance analysis for Gemini GTA-8 MISSION
Gemini VII star sightings analyzed, using handheld space sextant in Gemini VI, discussing effect of bias, timing angle measurement and trajectory errors
Bremsstrahlung flux-energy spectra inside Gemini 10 spacecraft during flight through south Atlantic magnetic anomaly region
Determination of meteorite activity outside Gemini 10 spacecraft by exposed metal plate
Ion and electron measurements in wake structure of orbiting Gemini 10 spacecraft
Space radiation environment shielding /Spares/ codes for determining radiation dosages on board Gemini 4 and Gemini 6 spacecrafts and in model environment
Procedures, ground equipment, and onboard equipment for optical communication experiment of Gemini 7 spacecraft
Navigation-type measurements through the window of the stabilized Gemini 12 spacecraft by the use of a hand-held sextant are reported. The major objectives were as follows: (1) to evaluate the ability of the crewmen to make accurate navigational measurements by the use of simple instruments in an authentic space flight environment; (2) to evaluate the operational feasibility of the measurement techniques by the use of the pressure suit with the helmet off and with the helmet on and the visor closed; (3) to evaluate operational problems associated with the spacecraft environment; and (4) to validate ground based simulation techniques by comparison of the inflight results with base line data obtained by the pilot by the use of simulators and celestial targets from ground based observatories.
Gemini launch vehicle, spacecraft systems, and performance data on reentry heating under maximum heating conditions
Vibration and acoustic tests on Mariner, Lunar Orbiter, Gemini, and Surveyor spacecraft