Preliminary Gemini 4 Crew Debriefing, Part II, 1965
NASA-UAP-D017 · page 233 of 290
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McDivitt 225 Cet-«:IDE~~TIAL~ limitations on hitting the side of the spacecraft and trying to make a sighting and losing the object out of the upper window as you cranked the periscope down to bring the star down to the horizon. In trying to accomplish the Air Force portion of the experiment, we found ourselves completely unable to do the daylight star-horizon measurement. So, to get some insight into the operational use of the sextant, we took a great number of star to horizon measurements at night. They are in the book in quite a bit of detail. As we mentioned earlier, the helmet was an impediment to use with the sextant, so on occasion we had to take the helmet off. The greatest angle that we ca~ld normally get was about 25 degrees between the horizon and the stars, but on occasion we got up to 30 degrees. This meant a certain alinement of the spacecraft was necessary so that you could get the largest piece of glass between the star and the horizon and still get the