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Gemini Ejection |
 | | The ejection seat was to provide the crew a means of escaping from the Gemini spacecraft in an emergency while the launch vehicle was still on the launch pad, during the initial phase of powered flight (to about 60,000 feet), or in case of paraglider failure after reentry. |
 | | In addition to the seat, the escape system included a hatch actuation system to open the hatches before ejection, a rocket catapult to propel the seat from the spacecraft, a personnel parachute system to sustain the astronaut after his separation from the seat, and survival equipment for the astronaut's use after landing. |
 | | The purpose of these simulated off-the-pad ejection tests was to investigate the effects of varying the center of gravity on the trajectory of the ejected seat and to optimize the timing of the recovery sequence. |
| www.astronautix.com /craft/gemction.htm (3023 words) |
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