Gemini flight control system performance during the second unmanned flight.
Gemini flight control system performance during second unmanned flight
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Gemini flight control system performance during second unmanned flight
Gemini manned space flight program
Analysis of brain wave records from Gemini flight GT-VII by computations to be used in 30-day primate flight
Gemini 4 manned orbital space flight - plan for launching, maneuvers, rendezvous, docking, and reentry
EEG data from Astronaut Borman on Gemini flight GT-7
Ground tracking reliability data for Gemini flights 9/9A, 10, 11, and 12
Gemini inflight experiments on space perception via measurements of ocular counterrolling as test of otolith function
Gemini 5 and 7 astronaut participation in otolith function experiments
Preflight medical predictions of space environment effects on spacecrews, and postflight analysis of Mercury and Gemini space flights
Analysis of baseline and Gemini GT-7 ELECTROENCEPHALOGRAM data with specification of on-line computing requirements
Final results from a part of the T027 experiment performed on the first Skylab mission are presented. The sample array system containing 248 optical surfaces and exposed outside the orbital workshop did not collect any significant contaminants. Unfortunate performance compromises and the relative cleanliness of the assembly on the antisolar side placed the amount of available surface contaminants at or below the limiting sensitivity of the ground measuring instruments. Significant contamination was seen near the extravehicular hatch quadrant on the solar side of the orbiting assembly, and some results from returned samples are presented. Optical windows and mirrors exposed on the Gemini 12 mission showed degradation up to 35% in the UV wavelength region and solar absorptance increases up to 1.8 times the clean values. An expression for the attenuation coefficient vs wavelength is presented. The contaminant, a silicone base material, varied in thickness from 22 nm to 88 nm. The postflight scattered luminance of a contaminated Gemini 12 left-hand spacecraft hatch window was used to obtain threshold stellar visibility curves as a function of scattered and incident sunlight angles.
Data analysis and display techniques for biosatellite flight and application of astronaut electroencephalogram analysis
Mission simulation techniques for training Gemini flight controllers
This compilation of papers constitutes an interim report on the results of experiments conducted during the Gemini V manned space flight. The results of experiments conducted on Gemini III and IV manned space flights have been published previously in a similar interim report, "Manned Space Flight Experiments Symposium, Gemini Missions III and IV," which is available upon request from MSC Experiments Program Office, Houston, Texas (Code EX, Attention of R. Kinard). The Gemini V mission provided the greatest opportunity to date for conducting experiments; the increased mission duration of eight days provided this added capability. The total mission experiment complement was seventeen. Five experiments were designed to obtain basic scientific knowledge, five were medical, and seven were technological and engineering in nature. Six of the experiments had flown previously on Gemini IV, and eleven were new. The results of the experiments, including real-time modification to preflight plans made necessary by abnormal spacecraft system operation, are presented.
Registration of heavy ions during flight of Gemini VI
Manned space flight research projects - Gemini and Apollo